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 28366U 26145.46251741 +.00000000 +00000-0 +51422-4 0 00004
2 28366 98.0997 312.7316 0104696 319.2349 40.1039 14.38026660 02
| Epoch (UTC): | 25 May 2026 11:06:01 |
| Eccentricity: | 0.0104696 |
| inclination: | 98.0997° |
| perigee height: | 690 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 312.7316° |
| argument of perigee: | 319.2349° |
| revolutions per day: | 14.38026660 |
| mean anomaly at epoch: | 40.1039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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