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 69042U 26145.58335647 +.00000000 +00000-0 -23415-1 0 00000
2 69042 97.2850 0.3842 0001519 75.8150 296.7253 15.71345215 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001519 |
| inclination: | 97.2850° |
| perigee height: | 354 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 0.3842° |
| argument of perigee: | 75.8150° |
| revolutions per day: | 15.71345215 |
| mean anomaly at epoch: | 296.7253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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