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 36796U 26156.30363332 +.00000000 +00000-0 +30706-3 0 00006
2 36796 98.0941 62.6822 0012452 74.8026 285.4575 15.04804368 06
| Epoch (UTC): | 05 June 2026 07:17:13 |
| Eccentricity: | 0.0012452 |
| inclination: | 98.0941° |
| perigee height: | 543 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 62.6822° |
| argument of perigee: | 74.8026° |
| revolutions per day: | 15.04804368 |
| mean anomaly at epoch: | 285.4575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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