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 42834U 26053.69811832 +.00000000 +00000-0 +42577-3 0 00006
2 42834 97.4074 219.2226 0010201 94.7910 265.4484 15.07759842 03
| Epoch (UTC): | 22 February 2026 16:45:17 |
| Eccentricity: | 0.0010201 |
| inclination: | 97.4074° |
| perigee height: | 536 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 219.2226° |
| argument of perigee: | 94.7910° |
| revolutions per day: | 15.07759842 |
| mean anomaly at epoch: | 265.4484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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