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 07578U 26017.81074007 +.00000000 +00000-0 +00000-0 0 00003
2 07578 4.9599 278.8966 0005309 6.4163 219.8382 0.99943542 06
| Epoch (UTC): | 17 January 2026 19:27:27 |
| Eccentricity: | 0.0005309 |
| inclination: | 4.9599° |
| perigee height: | 35856 km |
| apogee height: | 35901 km |
| right ascension of ascending node: | 278.8966° |
| argument of perigee: | 6.4163° |
| revolutions per day: | 0.99943542 |
| mean anomaly at epoch: | 219.8382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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