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 38771U 26053.80372062 +.00000000 +00000-0 +66816-4 0 00004
2 38771 98.6676 107.5021 0001567 340.1773 19.9343 14.21439251 01
| Epoch (UTC): | 22 February 2026 19:17:21 |
| Eccentricity: | 0.0001567 |
| inclination: | 98.6676° |
| perigee height: | 819 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 107.5021° |
| argument of perigee: | 340.1773° |
| revolutions per day: | 14.21439251 |
| mean anomaly at epoch: | 19.9343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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