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 42058U 17011A 26002.73681003 0.00000000 00000-0 00000-0 0 00
2 42058 63.4341 213.7344 0160236 0.1119 359.7624 13.40990371 09
| Epoch (UTC): | 02 January 2026 17:41:00 |
| Eccentricity: | 0.0160236 |
| inclination: | 63.4341° |
| perigee height: | 985 km |
| apogee height: | 1225 km |
| right ascension of ascending node: | 213.7344° |
| argument of perigee: | 0.1119° |
| revolutions per day: | 13.40990371 |
| mean anomaly at epoch: | 359.7624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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