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 28352U 26140.27665394 +.00000000 +00000-0 -16103-4 0 00004
2 28352 70.9929 157.8185 0010207 195.8016 164.2788 14.12132140 08
| Epoch (UTC): | 20 May 2026 06:38:22 |
| Eccentricity: | 0.0010207 |
| inclination: | 70.9929° |
| perigee height: | 845 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 157.8185° |
| argument of perigee: | 195.8016° |
| revolutions per day: | 14.12132140 |
| mean anomaly at epoch: | 164.2788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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