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 26067.89130994 +.00000000 +00000-0 -95082-4 0 00007
2 28353 70.9994 234.1679 0004001 10.7623 349.3584 14.14598290 06
| Epoch (UTC): | 08 March 2026 21:23:29 |
| Eccentricity: | 0.0004001 |
| inclination: | 70.9994° |
| perigee height: | 841 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 234.1679° |
| argument of perigee: | 10.7623° |
| revolutions per day: | 14.14598290 |
| mean anomaly at epoch: | 349.3584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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