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 42958U 26145.41387110 +.00000000 +00000-0 +74642-4 0 00001
2 42958 86.3990 34.7730 0002296 90.7190 269.4269 14.34219634 09
| Epoch (UTC): | 25 May 2026 09:55:58 |
| Eccentricity: | 0.0002296 |
| inclination: | 86.3990° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.7730° |
| argument of perigee: | 90.7190° |
| revolutions per day: | 14.34219634 |
| mean anomaly at epoch: | 269.4269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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