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 61630U 26145.51692019 +.00000000 +00000-0 -10695-4 0 00006
2 61630 42.9996 80.8382 0000850 264.0578 96.0176 15.27576442 03
| Epoch (UTC): | 25 May 2026 12:24:21 |
| Eccentricity: | 0.0000850 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.8382° |
| argument of perigee: | 264.0578° |
| revolutions per day: | 15.27576442 |
| mean anomaly at epoch: | 96.0176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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