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 61612U 26145.46430999 +.00000000 +00000-0 +18858-2 0 00003
2 61612 87.8862 40.7812 0001410 94.5651 265.5638 13.10374441 08
| Epoch (UTC): | 25 May 2026 11:08:36 |
| Eccentricity: | 0.0001410 |
| inclination: | 87.8862° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7812° |
| argument of perigee: | 94.5651° |
| revolutions per day: | 13.10374441 |
| mean anomaly at epoch: | 265.5638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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