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 52861U 26145.43223747 +.00000000 +00000-0 +61312-3 0 00001
2 52861 53.2126 39.6204 0001536 103.5090 256.6074 15.08796124 03
| Epoch (UTC): | 25 May 2026 10:22:25 |
| Eccentricity: | 0.0001536 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.6204° |
| argument of perigee: | 103.5090° |
| revolutions per day: | 15.08796124 |
| mean anomaly at epoch: | 256.6074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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