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 26104.13709925 +.00000000 +00000-0 +16325-3 0 00006
2 28897 98.2864 260.6192 0013949 38.3042 20.6602 14.73749386 03
| Epoch (UTC): | 14 April 2026 03:17:25 |
| Eccentricity: | 0.0013949 |
| inclination: | 98.2864° |
| perigee height: | 639 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 260.6192° |
| argument of perigee: | 38.3042° |
| revolutions per day: | 14.73749386 |
| mean anomaly at epoch: | 20.6602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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