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 28352U 26020.28148917 +.00000000 +00000-0 -10363-3 0 00000
2 28352 71.0053 48.6348 0011459 344.7855 15.2920 14.12162409 06
| Epoch (UTC): | 20 January 2026 06:45:20 |
| Eccentricity: | 0.0011459 |
| inclination: | 71.0053° |
| perigee height: | 844 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 48.6348° |
| argument of perigee: | 344.7855° |
| revolutions per day: | 14.12162409 |
| mean anomaly at epoch: | 15.2920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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