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 37841U 26145.47444316 +.00000000 +00000-0 +58040-4 0 00008
2 37841 19.9703 196.9483 0011657 315.1236 187.5474 14.11570120 03
| Epoch (UTC): | 25 May 2026 11:23:11 |
| Eccentricity: | 0.0011657 |
| inclination: | 19.9703° |
| perigee height: | 846 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 196.9483° |
| argument of perigee: | 315.1236° |
| revolutions per day: | 14.11570120 |
| mean anomaly at epoch: | 187.5474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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