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 26073.93795175 +.00000000 +00000-0 +10856-3 0 00003
2 37841 19.9715 269.9394 0011719 247.0003 267.6131 14.11549952 01
| Epoch (UTC): | 14 March 2026 22:30:39 |
| Eccentricity: | 0.0011719 |
| inclination: | 19.9715° |
| perigee height: | 846 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 269.9394° |
| argument of perigee: | 247.0003° |
| revolutions per day: | 14.11549952 |
| mean anomaly at epoch: | 267.6131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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