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 36036U 26150.46808896 +.00000000 +00000-0 +11681-3 0 00004
2 36036 98.4425 338.0628 0001322 92.4507 267.6833 14.39762256 07
| Epoch (UTC): | 30 May 2026 11:14:02 |
| Eccentricity: | 0.0001322 |
| inclination: | 98.4425° |
| perigee height: | 758 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 338.0628° |
| argument of perigee: | 92.4507° |
| revolutions per day: | 14.39762256 |
| mean anomaly at epoch: | 267.6833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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