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 68952U 26145.58335647 +.00000000 +00000-0 +32633-3 0 00002
2 68952 53.1593 268.7572 0001120 54.8845 70.8594 15.49287574 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1593° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 268.7572° |
| argument of perigee: | 54.8845° |
| revolutions per day: | 15.49287574 |
| mean anomaly at epoch: | 70.8594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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