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 26106.27459573 +.00000000 +00000-0 +43369-4 0 00009
2 28893 98.2758 240.2656 0015720 109.1368 251.1538 14.64113936 02
| Epoch (UTC): | 16 April 2026 06:35:25 |
| Eccentricity: | 0.0015720 |
| inclination: | 98.2758° |
| perigee height: | 669 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 240.2656° |
| argument of perigee: | 109.1368° |
| revolutions per day: | 14.64113936 |
| mean anomaly at epoch: | 251.1538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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