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 62181U 26145.45709510 +.00000000 +00000-0 +21534-3 0 00008
2 62181 70.0017 320.9072 0002382 271.9869 88.1017 14.98336368 01
| Epoch (UTC): | 25 May 2026 10:58:13 |
| Eccentricity: | 0.0002382 |
| inclination: | 70.0017° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 320.9072° |
| argument of perigee: | 271.9869° |
| revolutions per day: | 14.98336368 |
| mean anomaly at epoch: | 88.1017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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