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 26106.60801538 +.00000000 +00000-0 +87271-4 0 00004
2 00899 79.6922 194.3873 0118896 4.9034 355.3250 13.83036129 00
| Epoch (UTC): | 16 April 2026 14:35:32 |
| Eccentricity: | 0.0118896 |
| inclination: | 79.6922° |
| perigee height: | 866 km |
| apogee height: | 1040 km |
| right ascension of ascending node: | 194.3873° |
| argument of perigee: | 4.9034° |
| revolutions per day: | 13.83036129 |
| mean anomaly at epoch: | 355.3250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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