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 51648U 26145.43440819 +.00000000 +00000-0 -21094-2 0 00007
2 51648 87.8862 40.7870 0001986 78.2123 281.9227 13.10374242 06
| Epoch (UTC): | 25 May 2026 10:25:32 |
| Eccentricity: | 0.0001986 |
| inclination: | 87.8862° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7870° |
| argument of perigee: | 78.2123° |
| revolutions per day: | 13.10374242 |
| mean anomaly at epoch: | 281.9227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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