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 05678U 26088.03038993 +.00000000 +00000-0 +22825-4 0 00001
2 05678 69.9899 189.7415 0010727 280.4485 79.5400 13.74135118 00
| Epoch (UTC): | 29 March 2026 00:43:45 |
| Eccentricity: | 0.0010727 |
| inclination: | 69.9899° |
| perigee height: | 977 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 189.7415° |
| argument of perigee: | 280.4485° |
| revolutions per day: | 13.74135118 |
| mean anomaly at epoch: | 79.5400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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