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 00262U 26101.36971441 +.00000000 +00000-0 +38625-3 0 00005
2 00262 66.4612 250.3779 0052614 140.5697 219.9263 14.60036506 03
| Epoch (UTC): | 11 April 2026 08:52:23 |
| Eccentricity: | 0.0052614 |
| inclination: | 66.4612° |
| perigee height: | 656 km |
| apogee height: | 730 km |
| right ascension of ascending node: | 250.3779° |
| argument of perigee: | 140.5697° |
| revolutions per day: | 14.60036506 |
| mean anomaly at epoch: | 219.9263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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