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 48210U 26145.41977073 +.00000000 +00000-0 +23673-3 0 00008
2 48210 87.8945 294.2397 0001705 98.0506 262.0817 13.14502016 04
| Epoch (UTC): | 25 May 2026 10:04:28 |
| Eccentricity: | 0.0001705 |
| inclination: | 87.8945° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2397° |
| argument of perigee: | 98.0506° |
| revolutions per day: | 13.14502016 |
| mean anomaly at epoch: | 262.0817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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