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 68571U 26145.28392648 +.00000000 +00000-0 +00000-0 0 00000
2 68571 62.7926 231.7918 7191552 285.1363 11.1919 2.00618554 03
| Epoch (UTC): | 25 May 2026 06:48:51 |
| Eccentricity: | 0.7191552 |
| inclination: | 62.7926° |
| perigee height: | 1080 km |
| apogee height: | 39275 km |
| right ascension of ascending node: | 231.7918° |
| argument of perigee: | 285.1363° |
| revolutions per day: | 2.00618554 |
| mean anomaly at epoch: | 11.1919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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