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 68771U 26145.58335647 +.00000000 +00000-0 -23402-1 0 00004
2 68771 97.2847 182.4358 0001619 77.2652 53.4648 15.62437612 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001619 |
| inclination: | 97.2847° |
| perigee height: | 380 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 182.4358° |
| argument of perigee: | 77.2652° |
| revolutions per day: | 15.62437612 |
| mean anomaly at epoch: | 53.4648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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