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 02828U 26032.00630872 +.00000000 +00000-0 +84160-4 0 00005
2 02828 69.9728 355.4709 0008920 326.6775 33.3769 13.98054776 02
| Epoch (UTC): | 01 February 2026 00:09:05 |
| Eccentricity: | 0.0008920 |
| inclination: | 69.9728° |
| perigee height: | 894 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 355.4709° |
| argument of perigee: | 326.6775° |
| revolutions per day: | 13.98054776 |
| mean anomaly at epoch: | 33.3769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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