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 28097U 03054C 26002.79286449 0.00000300 00000-0 19968-3 0 09
2 28097 63.3900 251.9002 0577249 6.3998 353.6002 13.41262763 01
| Epoch (UTC): | 02 January 2026 19:01:43 |
| Eccentricity: | 0.0577249 |
| inclination: | 63.3900° |
| perigee height: | 672 km |
| apogee height: | 1536 km |
| right ascension of ascending node: | 251.9002° |
| argument of perigee: | 6.3998° |
| revolutions per day: | 13.41262763 |
| mean anomaly at epoch: | 353.6002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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