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 68739U 26145.58335647 +.00000000 +00000-0 -28276-1 0 00002
2 68739 97.2852 9.2068 0001676 84.2945 178.3028 15.51727867 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001676 |
| inclination: | 97.2852° |
| perigee height: | 411 km |
| apogee height: | 413 km |
| right ascension of ascending node: | 9.2068° |
| argument of perigee: | 84.2945° |
| revolutions per day: | 15.51727867 |
| mean anomaly at epoch: | 178.3028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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