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 44783U 26145.67813887 +.00000000 +00000-0 -33898-4 0 00001
2 44783 45.0060 279.7918 0010261 38.9974 321.1599 14.02084216 04
| Epoch (UTC): | 25 May 2026 16:16:31 |
| Eccentricity: | 0.0010261 |
| inclination: | 45.0060° |
| perigee height: | 879 km |
| apogee height: | 894 km |
| right ascension of ascending node: | 279.7918° |
| argument of perigee: | 38.9974° |
| revolutions per day: | 14.02084216 |
| mean anomaly at epoch: | 321.1599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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