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 26105.63924384 +.00000000 +00000-0 +39506-4 0 00008
2 36088 98.0017 88.4154 0009810 214.6889 199.7478 14.63626423 00
| Epoch (UTC): | 15 April 2026 15:20:30 |
| Eccentricity: | 0.0009810 |
| inclination: | 98.0017° |
| perigee height: | 675 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 88.4154° |
| argument of perigee: | 214.6889° |
| revolutions per day: | 14.63626423 |
| mean anomaly at epoch: | 199.7478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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