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 53701U 26145.35577602 +.00000000 +00000-0 -52165-4 0 00006
2 53701 53.2130 259.5403 0001281 95.2449 264.8689 15.08844419 02
| Epoch (UTC): | 25 May 2026 08:32:19 |
| Eccentricity: | 0.0001281 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 259.5403° |
| argument of perigee: | 95.2449° |
| revolutions per day: | 15.08844419 |
| mean anomaly at epoch: | 264.8689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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