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 51994U 26145.10603916 +.00000000 +00000-0 -51264-3 0 00007
2 51994 53.2127 36.0742 0001738 91.8576 268.2615 15.08880470 08
| Epoch (UTC): | 25 May 2026 02:32:41 |
| Eccentricity: | 0.0001738 |
| inclination: | 53.2127° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 36.0742° |
| argument of perigee: | 91.8576° |
| revolutions per day: | 15.08880470 |
| mean anomaly at epoch: | 268.2615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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