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 28908U 26160.54894156 +.00000000 +00000-0 +98071-4 0 00006
2 28908 82.4685 312.5445 0008179 179.9250 250.9554 12.55600546 08
| Epoch (UTC): | 09 June 2026 13:10:28 |
| Eccentricity: | 0.0008179 |
| inclination: | 82.4685° |
| perigee height: | 1435 km |
| apogee height: | 1448 km |
| right ascension of ascending node: | 312.5445° |
| argument of perigee: | 179.9250° |
| revolutions per day: | 12.55600546 |
| mean anomaly at epoch: | 250.9554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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