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 26071.99096373 +.00000000 +00000-0 -83966-4 0 00002
2 28352 70.9998 300.5682 0012129 279.6153 80.3598 14.12143907 01
| Epoch (UTC): | 12 March 2026 23:46:59 |
| Eccentricity: | 0.0012129 |
| inclination: | 70.9998° |
| perigee height: | 843 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 300.5682° |
| argument of perigee: | 279.6153° |
| revolutions per day: | 14.12143907 |
| mean anomaly at epoch: | 80.3598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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