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 61963U 26145.61498525 +.00000000 +00000-0 +75224-3 0 00009
2 61963 43.0011 105.4750 0001509 271.2307 88.8371 15.27590046 09
| Epoch (UTC): | 25 May 2026 14:45:34 |
| Eccentricity: | 0.0001509 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 105.4750° |
| argument of perigee: | 271.2307° |
| revolutions per day: | 15.27590046 |
| mean anomaly at epoch: | 88.8371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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