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 00899U 26106.24630950 +.00000000 +00000-0 +82657-4 0 00005
2 00899 79.6922 194.7830 0118911 5.8381 354.4122 13.83036077 00
| Epoch (UTC): | 16 April 2026 05:54:41 |
| Eccentricity: | 0.0118911 |
| inclination: | 79.6922° |
| perigee height: | 866 km |
| apogee height: | 1040 km |
| right ascension of ascending node: | 194.7830° |
| argument of perigee: | 5.8381° |
| revolutions per day: | 13.83036077 |
| mean anomaly at epoch: | 354.4122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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