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 52313U 26145.29831541 +.00000000 +00000-0 -40491-3 0 00000
2 52313 53.2136 105.2102 0001434 74.0835 286.0315 15.08874771 09
| Epoch (UTC): | 25 May 2026 07:09:34 |
| Eccentricity: | 0.0001434 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.2102° |
| argument of perigee: | 74.0835° |
| revolutions per day: | 15.08874771 |
| mean anomaly at epoch: | 286.0315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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