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 20978U 26146.17664692 +.00000000 +00000-0 +90143-4 0 00000
2 20978 98.6104 206.0123 0070735 351.5209 8.4778 14.40150586 05
| Epoch (UTC): | 26 May 2026 04:14:22 |
| Eccentricity: | 0.0070735 |
| inclination: | 98.6104° |
| perigee height: | 708 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 206.0123° |
| argument of perigee: | 351.5209° |
| revolutions per day: | 14.40150586 |
| mean anomaly at epoch: | 8.4778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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