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 51891U 26145.05268179 +.00000000 +00000-0 -96985-4 0 00005
2 51891 53.2134 16.3134 0001503 81.5941 278.5222 15.08851900 04
| Epoch (UTC): | 25 May 2026 01:15:51 |
| Eccentricity: | 0.0001503 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 16.3134° |
| argument of perigee: | 81.5941° |
| revolutions per day: | 15.08851900 |
| mean anomaly at epoch: | 278.5222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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