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 51108U 26145.15113355 +.00000000 +00000-0 +42615-5 0 00003
2 51108 53.2139 305.8718 0001435 93.1521 266.9635 15.08832896 03
| Epoch (UTC): | 25 May 2026 03:37:37 |
| Eccentricity: | 0.0001435 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 305.8718° |
| argument of perigee: | 93.1521° |
| revolutions per day: | 15.08832896 |
| mean anomaly at epoch: | 266.9635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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