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 26088.12996110 +.00000000 +00000-0 +11109-3 0 00009
2 36036 98.4435 276.6287 0000936 94.1194 266.0101 14.39773789 01
| Epoch (UTC): | 29 March 2026 03:07:08 |
| Eccentricity: | 0.0000936 |
| inclination: | 98.4435° |
| perigee height: | 759 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 276.6287° |
| argument of perigee: | 94.1194° |
| revolutions per day: | 14.39773789 |
| mean anomaly at epoch: | 266.0101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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