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 26150.65662749 +.00000000 +00000-0 +31384-3 0 00008
2 28897 98.2922 308.1566 0012180 242.8894 247.8975 14.73878101 08
| Epoch (UTC): | 30 May 2026 15:45:32 |
| Eccentricity: | 0.0012180 |
| inclination: | 98.2922° |
| perigee height: | 640 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 308.1566° |
| argument of perigee: | 242.8894° |
| revolutions per day: | 14.73878101 |
| mean anomaly at epoch: | 247.8975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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