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 51983U 26145.05269560 +.00000000 +00000-0 -13437-4 0 00003
2 51983 53.2133 56.3196 0001564 87.5769 272.5402 15.08840605 02
| Epoch (UTC): | 25 May 2026 01:15:52 |
| Eccentricity: | 0.0001564 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 56.3196° |
| argument of perigee: | 87.5769° |
| revolutions per day: | 15.08840605 |
| mean anomaly at epoch: | 272.5402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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