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
Defense Early Warn
Bus & Motor
MIDAS, Unknown motor
Mass
~1,540 kg wet, ~840 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + Cone, 4.5 m
Radar Cross Section
11.475 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 MIDAS 7/ERS 10
1 00622U 63030A 25258.42174018 .00000000 00000-0 -10125-2 0 9993
2 00622 88.4213 226.3652 0031365 335.5265 24.4095 8.57932485436212Epoch: 2025-09-15T10:07Z
TLE epoch observation values (Epoch: 2025-09-15T10:07:18.351Z)
Latitude
-0.00008°
Longitude
79.91211°
Altitude
3,674.632 km
Speed
6.307 km/s
True Right ascension
15h 05m 27s
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
23:07:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,730.66 km
Perigee altitude
3,667.446 km
Semi-major axis
10,077.19 km
Eccentricity
0.00314
Inclination
88.4213°
RAAN
226.3652°
Arg. of periapsis
335.5265°
True anomaly
24.55856°
Mean anomaly
24.4095°
Eccentric anomaly
24.48398°
Mean motion
2.14553 °/min
Orbital period
167.79 mins
BSTAR
-0.0010125
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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. |
|---|---|---|---|---|---|---|---|
| 18 mins | 2025-09-16 06:32:31.097Z | 20.991° NNE | 2025-09-16 06:41:31.097Z | 50.765° ENE | 13.818° | 2025-09-16 06:50:31.097Z | 80.538° E |
| 37 mins | 2025-09-16 09:17:31.097Z | 2.577° NNE | 2025-09-16 09:35:31.097Z | 82.111° E | 42.94° | 2025-09-16 09:54:31.097Z | 168.852° S |
| 30 mins | 2025-09-16 12:06:31.097Z | 348.583° N | 2025-09-16 12:21:31.097Z | 291.819° WNW | 30.319° | 2025-09-16 12:36:31.097Z | 236.98° WSW |
| 27 mins | 2025-09-16 19:50:31.097Z | 112.075° ESE | 2025-09-16 20:03:31.097Z | 64.539° ENE | 26.373° | 2025-09-16 20:17:31.097Z | 13.16° NNE |
| 37 mins | 2025-09-16 22:30:31.097Z | 183.705° SSW | 2025-09-16 22:48:31.097Z | 272.153° WNW | 44.417° | 2025-09-16 23:07:31.097Z | 359.481° N |
| 21 mins | 2025-09-17 01:31:31.097Z | 269.488° W | 2025-09-17 01:41:31.097Z | 304.685° NW | 17.199° | 2025-09-17 01:52:31.097Z | 342.403° N |
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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