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 00877U 26022.63494480 +.00000000 +00000-0 +15078-3 0 00009
2 00877 65.0771 106.2551 0077195 306.9094 52.4949 14.61315629 01
| Epoch (UTC): | 22 January 2026 15:14:19 |
| Eccentricity: | 0.0077195 |
| inclination: | 65.0771° |
| perigee height: | 634 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 106.2551° |
| argument of perigee: | 306.9094° |
| revolutions per day: | 14.61315629 |
| mean anomaly at epoch: | 52.4949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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