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 51639U 26145.43938904 +.00000000 +00000-0 -12142-2 0 00008
2 51639 87.8864 40.7820 0001651 84.3867 275.7449 13.10375862 01
| Epoch (UTC): | 25 May 2026 10:32:43 |
| Eccentricity: | 0.0001651 |
| inclination: | 87.8864° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7820° |
| argument of perigee: | 84.3867° |
| revolutions per day: | 13.10375862 |
| mean anomaly at epoch: | 275.7449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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