Showing default

VANGUARD 3, 20

Orbit data source: Space-Track

VANGUARD 3, 20 is a payload satellite owned by GSFC (US) in LEO that was launched on Fri, 18 Sep 1959 UTC via a VANGUARD launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
20, 1959-007A
Orbit
LEO
Last TLE update
9 hours ago
Origin
Manufacturer
NRL
Mission
Civil Science
Bus & Motor
NRL 20", Unknown motor
Mass
47 kg wet, 23 kg dry
Launch date (UTC)
1959-09-18 (66 years ago)
Launch vehicle
VANGUARD
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere + Cyl, 2.5 m
Radar Cross Section
1.104 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 9 hours ago
0 VANGUARD 3
1 00020U 59007A   25184.93664158  .00000867  00000-0  34935-3 0  9993
2 00020  33.3462  79.8608 1641979 347.8528   8.6636 11.60726810444112
Epoch: 2025-07-03T22:28Z
TLE epoch observation values (Epoch: 2025-07-03T22:28:45.832Z)
Latitude
-0.00005°
Longitude
-179.52647°
Altitude
529.89 km
Speed
8.189 km/s
True Right ascension
05h 19m 26s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
24.95022°
Longitude
-45.62327°
Altitude
2,796.469 km
Speed
6.21 km/s
Apparent Right ascension
11h 59m 44s
Apparent Declination
-1° 27' 45"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
19:15:33
Azimuth
281.293° WNW
Elevation
-15.393°
Doppler factor
1
Orbital elements
Apogee altitude
3,218.139 km
Perigee altitude
511.231 km
Semi-major axis
8,242.822 km
Eccentricity
0.1642
Inclination
33.3462°
RAAN
79.8608°
Arg. of periapsis
347.8528°
True anomaly
Unknown
Mean anomaly
8.6636°
Eccentric anomaly
Unknown
Mean motion
2.90021 °/min
Orbital period
124.13 mins
BSTAR
0.00034935
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #7 in the year 1959 (1959-09-18 UTC)

VANGUARD 3 Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
6 mins2025-07-04 19:18:46.608Z163.764° S2025-07-04 19:21:46.608Z132.091° SE13.782°2025-07-04 19:24:46.608Z108.315° ESE
15 mins2025-07-04 21:26:46.608Z221.782° SW2025-07-04 21:31:46.608Z150.624° SSE35.967°2025-07-04 21:41:46.608Z91.752° ESE
23 mins2025-07-04 23:35:46.608Z256.852° W2025-07-04 23:43:46.608Z175.667° S41.571°2025-07-04 23:58:46.608Z106.055° ESE
26 mins2025-07-05 01:47:46.608Z263.977° W2025-07-05 01:56:46.608Z204.131° SW37.277°2025-07-05 02:13:46.608Z133.093° SE
25 mins2025-07-05 04:00:46.608Z260.152° W2025-07-05 04:11:46.608Z213.206° SW24.514°2025-07-05 04:25:46.608Z167.047° S
|