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 26072.98265929 +.00000000 +00000-0 -81341-4 0 00002
2 28352 70.9995 298.4955 0012118 278.4468 81.5280 14.12143591 00
| Epoch (UTC): | 13 March 2026 23:35:01 |
| Eccentricity: | 0.0012118 |
| inclination: | 70.9995° |
| perigee height: | 843 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 298.4955° |
| argument of perigee: | 278.4468° |
| revolutions per day: | 14.12143591 |
| mean anomaly at epoch: | 81.5280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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