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 48216U 26145.39135788 +.00000000 +00000-0 +14134-3 0 00002
2 48216 87.8932 294.2597 0001487 109.1748 250.9542 13.14502395 08
| Epoch (UTC): | 25 May 2026 09:23:33 |
| Eccentricity: | 0.0001487 |
| inclination: | 87.8932° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2597° |
| argument of perigee: | 109.1748° |
| revolutions per day: | 13.14502395 |
| mean anomaly at epoch: | 250.9542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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