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 68724U 26145.58335647 +.00000000 +00000-0 -50369-1 0 00004
2 68724 53.1609 36.8405 0000998 91.7345 16.9377 15.39783749 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000998 |
| inclination: | 53.1609° |
| perigee height: | 446 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 36.8405° |
| argument of perigee: | 91.7345° |
| revolutions per day: | 15.39783749 |
| mean anomaly at epoch: | 16.9377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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