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 36582U 26052.31977442 +.00000000 +00000-0 +00000-0 0 00009
2 36582 0.0549 237.0623 0002443 97.8195 304.6735 1.00268233 02
| Epoch (UTC): | 21 February 2026 07:40:28 |
| Eccentricity: | 0.0002443 |
| inclination: | 0.0549° |
| perigee height: | 35777 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 237.0623° |
| argument of perigee: | 97.8195° |
| revolutions per day: | 1.00268233 |
| mean anomaly at epoch: | 304.6735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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