View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 48785U 26145.36576488 +.00000000 +00000-0 -23906-3 0 00004
2 48785 87.9003 263.7281 0001562 102.9017 257.2288 13.15549973 05
| Epoch (UTC): | 25 May 2026 08:46:42 |
| Eccentricity: | 0.0001562 |
| inclination: | 87.9003° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7281° |
| argument of perigee: | 102.9017° |
| revolutions per day: | 13.15549973 |
| mean anomaly at epoch: | 257.2288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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