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 55961U 26145.51886545 +.00000000 +00000-0 +76537-4 0 00001
2 55961 70.0005 70.6575 0002985 272.5333 87.5484 14.98328592 06
| Epoch (UTC): | 25 May 2026 12:27:09 |
| Eccentricity: | 0.0002985 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.6575° |
| argument of perigee: | 272.5333° |
| revolutions per day: | 14.98328592 |
| mean anomaly at epoch: | 87.5484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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