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 40553U 26053.83723656 +.00000000 +00000-0 -31437-3 0 00008
2 40553 82.4859 103.3486 0014214 232.6915 127.2870 12.42887735 04
| Epoch (UTC): | 22 February 2026 20:05:37 |
| Eccentricity: | 0.0014214 |
| inclination: | 82.4859° |
| perigee height: | 1483 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 103.3486° |
| argument of perigee: | 232.6915° |
| revolutions per day: | 12.42887735 |
| mean anomaly at epoch: | 127.2870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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