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 26103.17961551 +.00000000 +00000-0 +00000-0 0 00004
2 36582 0.0099 203.6189 0002756 195.4898 240.0829 1.00271604 03
| Epoch (UTC): | 13 April 2026 04:18:38 |
| Eccentricity: | 0.0002756 |
| inclination: | 0.0099° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 203.6189° |
| argument of perigee: | 195.4898° |
| revolutions per day: | 1.00271604 |
| mean anomaly at epoch: | 240.0829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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