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 61613U 26145.40620634 +.00000000 +00000-0 +79272-3 0 00003
2 61613 87.8850 40.8131 0002140 94.0315 266.1057 13.10371139 07
| Epoch (UTC): | 25 May 2026 09:44:56 |
| Eccentricity: | 0.0002140 |
| inclination: | 87.8850° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8131° |
| argument of perigee: | 94.0315° |
| revolutions per day: | 13.10371139 |
| mean anomaly at epoch: | 266.1057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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