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 01778U 26088.17966608 +.00000000 +00000-0 +79544-4 0 00006
2 01778 34.2563 261.7419 0739863 353.9368 5.2718 13.49754279 05
| Epoch (UTC): | 29 March 2026 04:18:43 |
| Eccentricity: | 0.0739863 |
| inclination: | 34.2563° |
| perigee height: | 522 km |
| apogee height: | 1624 km |
| right ascension of ascending node: | 261.7419° |
| argument of perigee: | 353.9368° |
| revolutions per day: | 13.49754279 |
| mean anomaly at epoch: | 5.2718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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