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 42962U 26145.43924301 +.00000000 +00000-0 +19752-4 0 00008
2 42962 86.3990 34.7654 0002291 84.3433 275.8024 14.34217262 08
| Epoch (UTC): | 25 May 2026 10:32:30 |
| Eccentricity: | 0.0002291 |
| inclination: | 86.3990° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.7654° |
| argument of perigee: | 84.3433° |
| revolutions per day: | 14.34217262 |
| mean anomaly at epoch: | 275.8024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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