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 28912U 26113.93617779 +.00000000 +00000-0 +00000-0 0 00007
2 28912 9.2420 54.6903 0000373 346.0252 193.9141 1.00273321 00
| Epoch (UTC): | 23 April 2026 22:28:05 |
| Eccentricity: | 0.0000373 |
| inclination: | 9.2420° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 54.6903° |
| argument of perigee: | 346.0252° |
| revolutions per day: | 1.00273321 |
| mean anomaly at epoch: | 193.9141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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