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 53709U 26145.29829352 +.00000000 +00000-0 -56073-4 0 00001
2 53709 53.2151 264.9049 0001204 94.7536 265.3594 15.08831775 07
| Epoch (UTC): | 25 May 2026 07:09:32 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 264.9049° |
| argument of perigee: | 94.7536° |
| revolutions per day: | 15.08831775 |
| mean anomaly at epoch: | 265.3594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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