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 28897U 26160.14634382 +.00000000 +00000-0 +23270-3 0 00000
2 28897 98.2934 317.8584 0012666 210.6269 202.6950 14.73912621 04
| Epoch (UTC): | 09 June 2026 03:30:44 |
| Eccentricity: | 0.0012666 |
| inclination: | 98.2934° |
| perigee height: | 640 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 317.8584° |
| argument of perigee: | 210.6269° |
| revolutions per day: | 14.73912621 |
| mean anomaly at epoch: | 202.6950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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