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 61980U 26145.37528634 +.00000000 +00000-0 +63807-3 0 00000
2 61980 42.9998 107.1191 0001325 266.5889 93.4811 15.27588628 00
| Epoch (UTC): | 25 May 2026 09:00:24 |
| Eccentricity: | 0.0001325 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.1191° |
| argument of perigee: | 266.5889° |
| revolutions per day: | 15.27588628 |
| mean anomaly at epoch: | 93.4811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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