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 26106.23675397 +.00000000 +00000-0 +52901-4 0 00004
2 37841 19.9721 74.4374 0011613 241.6849 237.7724 14.11560608 03
| Epoch (UTC): | 16 April 2026 05:40:55 |
| Eccentricity: | 0.0011613 |
| inclination: | 19.9721° |
| perigee height: | 846 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 74.4374° |
| argument of perigee: | 241.6849° |
| revolutions per day: | 14.11560608 |
| mean anomaly at epoch: | 237.7724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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