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 51644U 26145.57817769 +.00000000 +00000-0 -54354-4 0 00007
2 51644 87.9153 10.3762 0002118 80.3158 279.8213 13.17649550 04
| Epoch (UTC): | 25 May 2026 13:52:34 |
| Eccentricity: | 0.0002118 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3762° |
| argument of perigee: | 80.3158° |
| revolutions per day: | 13.17649550 |
| mean anomaly at epoch: | 279.8213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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