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 61962U 26145.24373094 +.00000000 +00000-0 +54911-3 0 00000
2 61962 43.0037 93.1462 0001425 259.0180 101.0512 15.27598836 09
| Epoch (UTC): | 25 May 2026 05:50:58 |
| Eccentricity: | 0.0001425 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 93.1462° |
| argument of perigee: | 259.0180° |
| revolutions per day: | 15.27598836 |
| mean anomaly at epoch: | 101.0512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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