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 36108U 26063.12472088 +.00000000 +00000-0 +00000-0 0 00000
2 36108 0.3532 86.3241 0002138 310.0467 7.3204 1.00962160 03
| Epoch (UTC): | 04 March 2026 02:59:35 |
| Eccentricity: | 0.0002138 |
| inclination: | 0.3532° |
| perigee height: | 35585 km |
| apogee height: | 35603 km |
| right ascension of ascending node: | 86.3241° |
| argument of perigee: | 310.0467° |
| revolutions per day: | 1.00962160 |
| mean anomaly at epoch: | 7.3204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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