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 62262U 26145.41289918 +.00000000 +00000-0 +42824-3 0 00004
2 62262 53.1604 223.3497 0001215 121.4563 238.6557 15.30204594 09
| Epoch (UTC): | 25 May 2026 09:54:34 |
| Eccentricity: | 0.0001215 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.3497° |
| argument of perigee: | 121.4563° |
| revolutions per day: | 15.30204594 |
| mean anomaly at epoch: | 238.6557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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