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 26021.53995889 +.00000000 +00000-0 +14717-3 0 00005
2 00877 65.0771 109.4650 0077117 307.2599 52.1484 14.61313864 04
| Epoch (UTC): | 21 January 2026 12:57:32 |
| Eccentricity: | 0.0077117 |
| inclination: | 65.0771° |
| perigee height: | 634 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 109.4650° |
| argument of perigee: | 307.2599° |
| revolutions per day: | 14.61313864 |
| mean anomaly at epoch: | 52.1484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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