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 28890U 26145.58897208 +.00000000 +00000-0 +51508-4 0 00008
2 28890 98.2878 278.6800 0014579 357.7927 2.3208 14.63516347 03
| Epoch (UTC): | 25 May 2026 14:08:07 |
| Eccentricity: | 0.0014579 |
| inclination: | 98.2878° |
| perigee height: | 672 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 278.6800° |
| argument of perigee: | 357.7927° |
| revolutions per day: | 14.63516347 |
| mean anomaly at epoch: | 2.3208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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