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 69100U 26135.89543416 +.00000000 +00000-0 +33645-4 0 00001
2 69100 97.5062 218.5717 0012136 280.2995 79.6866 15.10959134 06
| Epoch (UTC): | 15 May 2026 21:29:25 |
| Eccentricity: | 0.0012136 |
| inclination: | 97.5062° |
| perigee height: | 525 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 218.5717° |
| argument of perigee: | 280.2995° |
| revolutions per day: | 15.10959134 |
| mean anomaly at epoch: | 79.6866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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