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 36797U 26150.50098610 +.00000000 +00000-0 +23035-3 0 00004
2 36797 98.0939 49.1219 0009889 112.2006 248.0264 14.97274746 01
| Epoch (UTC): | 30 May 2026 12:01:25 |
| Eccentricity: | 0.0009889 |
| inclination: | 98.0939° |
| perigee height: | 568 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 49.1219° |
| argument of perigee: | 112.2006° |
| revolutions per day: | 14.97274746 |
| mean anomaly at epoch: | 248.0264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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