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 37794U 26141.22301686 +.00000000 +00000-0 +74600-4 0 00006
2 37794 97.8365 123.0175 0010571 254.3492 116.2720 14.65607263 01
| Epoch (UTC): | 21 May 2026 05:21:08 |
| Eccentricity: | 0.0010571 |
| inclination: | 97.8365° |
| perigee height: | 668 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 123.0175° |
| argument of perigee: | 254.3492° |
| revolutions per day: | 14.65607263 |
| mean anomaly at epoch: | 116.2720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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