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 26382U 26053.53838105 +.00000000 +00000-0 +00000-0 0 00003
2 26382 13.1582 17.7462 0004108 292.5867 80.9553 1.00075833 09
| Epoch (UTC): | 22 February 2026 12:55:16 |
| Eccentricity: | 0.0004108 |
| inclination: | 13.1582° |
| perigee height: | 35824 km |
| apogee height: | 35859 km |
| right ascension of ascending node: | 17.7462° |
| argument of perigee: | 292.5867° |
| revolutions per day: | 1.00075833 |
| mean anomaly at epoch: | 80.9553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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