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 51865U 26145.07384491 +.00000000 +00000-0 -61189-4 0 00002
2 51865 53.2154 26.2170 0001335 106.8595 253.2544 15.08845233 05
| Epoch (UTC): | 25 May 2026 01:46:20 |
| Eccentricity: | 0.0001335 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 26.2170° |
| argument of perigee: | 106.8595° |
| revolutions per day: | 15.08845233 |
| mean anomaly at epoch: | 253.2544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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