SWIFT, 28485
Orbit data source: Space-Track
SWIFT, 28485 is a payload satellite owned by GSFC (US) in LEO that was launched on Sat, 20 Nov 2004 UTC via a DELTA 7320-10C 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.
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28485 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
GD C4 Systems
Mission
Operational Civil Astronomy
Bus & Motor
SA-200HP, Unknown motor
Mass
1,470 kg wet, 1,470 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 8.7 m
Radar Cross Section
6.084 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 SWIFT
1 28485U 04047A 26002.18758869 .00070726 00000-0 10911-2 0 9990
2 28485 20.5555 10.7446 0004838 180.2195 179.8246 15.52418305160897Epoch: 2026-01-02T04:30Z
TLE epoch observation values (Epoch: 2026-01-02T04:30:07.662Z)
Latitude
-0.00003°
Longitude
-158.61879°
Altitude
410.516 km
Speed
7.666 km/s
True Right ascension
00h 42m 58s
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
09:17:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
418.25 km
Perigee altitude
411.677 km
Semi-major axis
6,793.1 km
Eccentricity
0.00048
Inclination
20.5555°
RAAN
10.7446°
Arg. of periapsis
180.2195°
True anomaly
179.82477°
Mean anomaly
179.8246°
Eccentric anomaly
179.82468°
Mean motion
3.87651 °/min
Orbital period
92.87 mins
BSTAR
0.0010911
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Other satellites on launch #47 in the year 2004 (2004-11-20 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SWIFT Visibility
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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. |
|---|---|---|---|---|---|---|---|
| SWIFT is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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