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 45096U 26145.41538071 +.00000000 +00000-0 +98823-3 0 00007
2 45096 53.0346 202.0496 0004070 23.7001 336.4192 15.47106540 05
| Epoch (UTC): | 25 May 2026 09:58:08 |
| Eccentricity: | 0.0004070 |
| inclination: | 53.0346° |
| perigee height: | 422 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 202.0496° |
| argument of perigee: | 23.7001° |
| revolutions per day: | 15.47106540 |
| mean anomaly at epoch: | 336.4192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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