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 53707U 26144.99473016 +.00000000 +00000-0 +26791-4 0 00000
2 53707 53.2161 246.5870 0001212 88.3068 271.8063 15.08837918 00
| Epoch (UTC): | 24 May 2026 23:52:24 |
| Eccentricity: | 0.0001212 |
| inclination: | 53.2161° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 246.5870° |
| argument of perigee: | 88.3068° |
| revolutions per day: | 15.08837918 |
| mean anomaly at epoch: | 271.8063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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