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 36088U 26042.27520516 +.00000000 +00000-0 +17052-3 0 00008
2 36088 97.9945 26.9263 0012286 62.4935 54.1102 14.63524431 02
| Epoch (UTC): | 11 February 2026 06:36:17 |
| Eccentricity: | 0.0012286 |
| inclination: | 97.9945° |
| perigee height: | 673 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 26.9263° |
| argument of perigee: | 62.4935° |
| revolutions per day: | 14.63524431 |
| mean anomaly at epoch: | 54.1102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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