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 26037.82863455 +.00000000 +00000-0 +16723-3 0 00000
2 36089 98.4424 14.6862 0079276 80.2420 280.7717 14.52287321 00
| Epoch (UTC): | 06 February 2026 19:53:14 |
| Eccentricity: | 0.0079276 |
| inclination: | 98.4424° |
| perigee height: | 662 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 14.6862° |
| argument of perigee: | 80.2420° |
| revolutions per day: | 14.52287321 |
| mean anomaly at epoch: | 280.7717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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