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 51795U 26145.02418963 +.00000000 +00000-0 +28743-4 0 00009
2 51795 53.2147 6.6404 0001417 93.2477 266.8677 15.08839236 03
| Epoch (UTC): | 25 May 2026 00:34:49 |
| Eccentricity: | 0.0001417 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 6.6404° |
| argument of perigee: | 93.2477° |
| revolutions per day: | 15.08839236 |
| mean anomaly at epoch: | 266.8677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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