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 42610U 26053.90472801 +.00000000 +00000-0 -27752-5 0 00002
2 42610 101.4125 287.4740 0079709 346.4303 13.4621 12.40361398 00
| Epoch (UTC): | 22 February 2026 21:42:48 |
| Eccentricity: | 0.0079709 |
| inclination: | 101.4125° |
| perigee height: | 1442 km |
| apogee height: | 1568 km |
| right ascension of ascending node: | 287.4740° |
| argument of perigee: | 346.4303° |
| revolutions per day: | 12.40361398 |
| mean anomaly at epoch: | 13.4621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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