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 61789U 26145.51460492 +.00000000 +00000-0 +26053-3 0 00002
2 61789 97.3262 346.5418 0007414 136.0155 224.1659 14.97821866 01
| Epoch (UTC): | 25 May 2026 12:21:01 |
| Eccentricity: | 0.0007414 |
| inclination: | 97.3262° |
| perigee height: | 568 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 346.5418° |
| argument of perigee: | 136.0155° |
| revolutions per day: | 14.97821866 |
| mean anomaly at epoch: | 224.1659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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