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 26155.21093431 +.00000000 +00000-0 +00000-0 0 00009
2 36582 0.0126 3.9101 0003323 86.8436 251.0832 1.00277692 00
| Epoch (UTC): | 04 June 2026 05:03:44 |
| Eccentricity: | 0.0003323 |
| inclination: | 0.0126° |
| perigee height: | 35771 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 3.9101° |
| argument of perigee: | 86.8436° |
| revolutions per day: | 1.00277692 |
| mean anomaly at epoch: | 251.0832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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