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 28893U 26150.83261205 +.00000000 +00000-0 +86747-4 0 00000
2 28893 98.2837 285.0548 0013777 335.4620 24.5925 14.64144457 06
| Epoch (UTC): | 30 May 2026 19:58:57 |
| Eccentricity: | 0.0013777 |
| inclination: | 98.2837° |
| perigee height: | 670 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 285.0548° |
| argument of perigee: | 335.4620° |
| revolutions per day: | 14.64144457 |
| mean anomaly at epoch: | 24.5925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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