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 36599U 26032.48394984 +.00000000 +00000-0 +15610-3 0 00003
2 36599 98.0270 236.6245 0051664 271.1104 88.4177 14.58997565 00
| Epoch (UTC): | 01 February 2026 11:36:53 |
| Eccentricity: | 0.0051664 |
| inclination: | 98.0270° |
| perigee height: | 660 km |
| apogee height: | 733 km |
| right ascension of ascending node: | 236.6245° |
| argument of perigee: | 271.1104° |
| revolutions per day: | 14.58997565 |
| mean anomaly at epoch: | 88.4177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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