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 28353U 26070.86123670 +.00000000 +00000-0 -11320-3 0 00003
2 28353 70.9996 227.9350 0004176 6.1397 353.9776 14.14597110 08
| Epoch (UTC): | 11 March 2026 20:40:10 |
| Eccentricity: | 0.0004176 |
| inclination: | 70.9996° |
| perigee height: | 841 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 227.9350° |
| argument of perigee: | 6.1397° |
| revolutions per day: | 14.14597110 |
| mean anomaly at epoch: | 353.9776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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