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 28373U 26100.00168389 +.00000000 +00000-0 +12156-3 0 00008
2 28373 98.6965 107.7897 0064890 197.3315 162.5662 14.49012809 09
| Epoch (UTC): | 10 April 2026 00:02:25 |
| Eccentricity: | 0.0064890 |
| inclination: | 98.6965° |
| perigee height: | 683 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 107.7897° |
| argument of perigee: | 197.3315° |
| revolutions per day: | 14.49012809 |
| mean anomaly at epoch: | 162.5662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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