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 60945U 26145.63102170 +.00000000 +00000-0 +85297-3 0 00009
2 60945 34.9953 300.2529 0003467 52.7560 307.3478 15.47531269 00
| Epoch (UTC): | 25 May 2026 15:08:40 |
| Eccentricity: | 0.0003467 |
| inclination: | 34.9953° |
| perigee height: | 422 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 300.2529° |
| argument of perigee: | 52.7560° |
| revolutions per day: | 15.47531269 |
| mean anomaly at epoch: | 307.3478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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