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 68716U 26144.99849804 +.00000000 +00000-0 +12404-2 0 00002
2 68716 53.1597 40.5433 0000991 90.7001 269.4121 15.49328958 04
| Epoch (UTC): | 24 May 2026 23:57:50 |
| Eccentricity: | 0.0000991 |
| inclination: | 53.1597° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 40.5433° |
| argument of perigee: | 90.7001° |
| revolutions per day: | 15.49328958 |
| mean anomaly at epoch: | 269.4121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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