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 26075.87747265 +.00000000 +00000-0 +54089-4 0 00001
2 00877 65.0773 310.1647 0080011 289.9593 69.2902 14.61373679 04
| Epoch (UTC): | 16 March 2026 21:03:33 |
| Eccentricity: | 0.0080011 |
| inclination: | 65.0773° |
| perigee height: | 632 km |
| apogee height: | 745 km |
| right ascension of ascending node: | 310.1647° |
| argument of perigee: | 289.9593° |
| revolutions per day: | 14.61373679 |
| mean anomaly at epoch: | 69.2902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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