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 37793U 26159.74653558 +.00000000 +00000-0 +11682-3 0 00009
2 37793 98.2371 70.0737 0044341 112.2528 312.6846 14.76904004 07
| Epoch (UTC): | 08 June 2026 17:55:00 |
| Eccentricity: | 0.0044341 |
| inclination: | 98.2371° |
| perigee height: | 608 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 70.0737° |
| argument of perigee: | 112.2528° |
| revolutions per day: | 14.76904004 |
| mean anomaly at epoch: | 312.6846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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