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 68700U 26145.50003470 +.00000000 +00000-0 -69719-1 0 00005
2 68700 53.1600 37.6671 0001583 83.3875 71.3152 15.37393310 03
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001583 |
| inclination: | 53.1600° |
| perigee height: | 453 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 37.6671° |
| argument of perigee: | 83.3875° |
| revolutions per day: | 15.37393310 |
| mean anomaly at epoch: | 71.3152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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