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 28375U 26152.13595069 +.00000000 +00000-0 +74639-4 0 00005
2 28375 98.6606 115.8229 0080368 165.3240 195.0310 14.43865015 02
| Epoch (UTC): | 01 June 2026 03:15:46 |
| Eccentricity: | 0.0080368 |
| inclination: | 98.6606° |
| perigee height: | 689 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 115.8229° |
| argument of perigee: | 165.3240° |
| revolutions per day: | 14.43865015 |
| mean anomaly at epoch: | 195.0310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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