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 36600U 26088.19605843 +.00000000 +00000-0 +33696-4 0 00009
2 36600 98.2671 312.7875 0375166 99.3492 11.7770 13.72789477 05
| Epoch (UTC): | 29 March 2026 04:42:19 |
| Eccentricity: | 0.0375166 |
| inclination: | 98.2671° |
| perigee height: | 713 km |
| apogee height: | 1266 km |
| right ascension of ascending node: | 312.7875° |
| argument of perigee: | 99.3492° |
| revolutions per day: | 13.72789477 |
| mean anomaly at epoch: | 11.7770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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