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VANGUARD 1

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VANGUARD 1 is classified as:


NORAD ID: 5
Int'l Code: 1958-002B
Perigee: 28,068.8 km
Apogee: 43,671.5 km
Inclination: 34.2 °
Period: 1,440.0 minutes
Semi major axis: 42241 km
RCS: 0.118 m2 (medium)
Launch date: March 17, 1958
Source: United States (US)
Launch site: AIR FORCE EASTERN TEST RANGE (AFETR)

Vanguard 1 was a small earth-orbiting satellite designed to test the launch capabilities of a three-stage launch vehicle and the effects of the environment on a satellite and its systems in Earth orbit. It also was used to obtain geodetic measurements through orbit analysis.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 00005U 58002B   16037.46761952  .00000096  00000-0  14090-3 0  9999
2 00005  34.2459  94.8478 1846861  24.8850 343.0446 1.84735651 32352
Source of the keplerian elements: AFSPC

N2YO: 553