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 36089U 26065.38702727 +.00000000 +00000-0 +21752-3 0 00004
2 36089 98.4474 42.4072 0077957 356.7276 3.3399 14.52323420 07
| Epoch (UTC): | 06 March 2026 09:17:19 |
| Eccentricity: | 0.0077957 |
| inclination: | 98.4474° |
| perigee height: | 663 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 42.4072° |
| argument of perigee: | 356.7276° |
| revolutions per day: | 14.52323420 |
| mean anomaly at epoch: | 3.3399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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