MIDAS 7/ERS 10, 622
Orbit data source: Space-Track
MIDAS 7/ERS 10, 622 is a payload satellite owned by USAF SSD (US) in LEO that was launched on Fri, 19 Jul 1963 UTC via an ATLAS AGENA B launch vehicle from the Air Force Western Test Range (AFWTR). 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
LMSC
Mission
Spacecraft
Bus & Motor
MIDAS, Unknown motor
Mass
~1,540 kg wet, ~840 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 MIDAS 7/ERS 10
1 622U 63030A 25298.18127917 .00000021 00000-0 93860-2 0 9995
2 622 88.4318 224.1804 0030894 295.7051 64.0611 8.57932393439629Epoch: 2025-10-25T04:21Z
TLE epoch observation values (Epoch: 2025-10-25T04:21:02.520Z)
Latitude
0.00002°
Longitude
125.10439°
Altitude
3,689.863 km
Speed
6.297 km/s
True Right ascension
14h 56m 43s
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
17:08:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,730.186 km
Perigee altitude
3,667.921 km
Semi-major axis
10,077.191 km
Eccentricity
0.00309
Inclination
88.4318°
RAAN
224.1804°
Arg. of periapsis
295.7051°
True anomaly
64.37999°
Mean anomaly
64.0611°
Eccentric anomaly
64.22049°
Mean motion
2.14553 °/min
Orbital period
167.79 mins
BSTAR
0.009386
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Other satellites on launch #30 in the year 1963 (1963-07-19 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.MIDAS 7/ERS 10 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-10-26 03:36:34.709Z | 28.449° NE | 2025-10-26 03:42:34.709Z | 48.087° ENE | 11.822° | 2025-10-26 03:48:34.709Z | 67.644° E |
| 36 mins | 2025-10-26 06:19:34.709Z | 3.806° NNE | 2025-10-26 06:37:34.709Z | 84.845° E | 41.648° | 2025-10-26 06:55:34.709Z | 163.503° S |
| 31 mins | 2025-10-26 09:08:34.709Z | 349.031° N | 2025-10-26 09:23:34.709Z | 290.627° WNW | 32.571° | 2025-10-26 09:39:34.709Z | 231.078° WSW |
| 26 mins | 2025-10-26 16:53:34.709Z | 105.787° ESE | 2025-10-26 17:06:34.709Z | 58.569° ENE | 24.162° | 2025-10-26 17:19:34.709Z | 13.249° NNE |
| 37 mins | 2025-10-26 19:32:34.709Z | 178.868° S | 2025-10-26 19:50:34.709Z | 292.81° NW | 44.861° | 2025-10-26 20:09:34.709Z | 0.349° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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