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 26087.97371557 +.00000000 +00000-0 +12940-3 0 00000
2 28353 71.0009 192.0242 0004983 346.2595 13.8391 14.14595002 04
| Epoch (UTC): | 28 March 2026 23:22:09 |
| Eccentricity: | 0.0004983 |
| inclination: | 71.0009° |
| perigee height: | 840 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 192.0242° |
| argument of perigee: | 346.2595° |
| revolutions per day: | 14.14595002 |
| mean anomaly at epoch: | 13.8391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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