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 36597U 26074.32085104 +.00000000 +00000-0 +15924-3 0 00009
2 36597 97.9899 100.7269 0047767 233.1628 126.5210 15.02360746 05
| Epoch (UTC): | 15 March 2026 07:42:01 |
| Eccentricity: | 0.0047767 |
| inclination: | 97.9899° |
| perigee height: | 526 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 100.7269° |
| argument of perigee: | 233.1628° |
| revolutions per day: | 15.02360746 |
| mean anomaly at epoch: | 126.5210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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