SNOOPI, 59563 (Decayed)
Orbit data source: Space-Track
SNOOPI, 59563 was an American payload satellite in LEO that was delivered to the ISS. 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.
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59563 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
GSFC/PURDUE
Mission
Decayed spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 SNOOPI
1 59563U 98067WN 24269.79580319 .02239490 64862-2 16132-2 0 9995
2 59563 51.6152 156.6182 0007784 233.6043 126.4257 16.16734086 25169Epoch: 2024-09-25T19:05Z
TLE epoch observation values (Epoch: 2024-09-25T19:05:57.395Z)
Latitude
0.00002°
Longitude
-134.96143°
Altitude
232.25 km
Speed
7.767 km/s
True Right ascension
10h 26m 28s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:59:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
234.103 km
Perigee altitude
223.817 km
Semi-major axis
6,607.097 km
Eccentricity
0.00078
Inclination
51.6152°
RAAN
156.6182°
Arg. of periapsis
233.6043°
True anomaly
126.49743°
Mean anomaly
126.4257°
Eccentric anomaly
126.46157°
Mean motion
4.04136 °/min
Orbital period
89.08 mins
BSTAR
0.0016132
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Other satellites on launch #67 in the year 1998 (1998-11-20 UTC)
SNOOPI Visibility
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. |
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Authenticating...
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