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 26032.05368595 +.00000000 +00000-0 +41875-4 0 00002
2 05678 69.9906 305.1428 0008727 335.8068 24.2615 13.74130870 01
| Epoch (UTC): | 01 February 2026 01:17:18 |
| Eccentricity: | 0.0008727 |
| inclination: | 69.9906° |
| perigee height: | 978 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 305.1428° |
| argument of perigee: | 335.8068° |
| revolutions per day: | 13.74130870 |
| mean anomaly at epoch: | 24.2615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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