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 61561U 26145.60738801 +.00000000 +00000-0 +23877-3 0 00003
2 61561 88.9855 57.7331 0009484 102.4454 257.7803 14.28349616 01
| Epoch (UTC): | 25 May 2026 14:34:38 |
| Eccentricity: | 0.0009484 |
| inclination: | 88.9855° |
| perigee height: | 790 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 57.7331° |
| argument of perigee: | 102.4454° |
| revolutions per day: | 14.28349616 |
| mean anomaly at epoch: | 257.7803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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