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 26075.82161683 +.00000000 +00000-0 +95439-4 0 00005
2 37841 19.9713 258.5379 0011707 267.8502 119.4783 14.11550620 08
| Epoch (UTC): | 16 March 2026 19:43:07 |
| Eccentricity: | 0.0011707 |
| inclination: | 19.9713° |
| perigee height: | 846 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 258.5379° |
| argument of perigee: | 267.8502° |
| revolutions per day: | 14.11550620 |
| mean anomaly at epoch: | 119.4783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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