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 26139.86133162 +.00000000 +00000-0 +43738-4 0 00009
2 36089 98.4553 117.4068 0078900 127.3473 233.4944 14.52382264 06
| Epoch (UTC): | 19 May 2026 20:40:19 |
| Eccentricity: | 0.0078900 |
| inclination: | 98.4553° |
| perigee height: | 662 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 117.4068° |
| argument of perigee: | 127.3473° |
| revolutions per day: | 14.52382264 |
| mean anomaly at epoch: | 233.4944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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