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 62072U 26145.58335647 +.00000000 +00000-0 +10324-2 0 00001
2 62072 53.1593 196.8368 0001057 89.9476 234.6022 15.33514602 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001057 |
| inclination: | 53.1593° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 196.8368° |
| argument of perigee: | 89.9476° |
| revolutions per day: | 15.33514602 |
| mean anomaly at epoch: | 234.6022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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