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 36605U 26051.60485828 +.00000000 +00000-0 +47298-4 0 00002
2 36605 97.4470 60.9712 0001927 100.4407 259.7044 15.19148615 05
| Epoch (UTC): | 20 February 2026 14:30:59 |
| Eccentricity: | 0.0001927 |
| inclination: | 97.4470° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 60.9712° |
| argument of perigee: | 100.4407° |
| revolutions per day: | 15.19148615 |
| mean anomaly at epoch: | 259.7044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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