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 26072.41691378 +.00000000 +00000-0 -12159-3 0 00002
2 28353 70.9996 224.6701 0004293 3.8877 356.2278 14.14596418 02
| Epoch (UTC): | 13 March 2026 10:00:21 |
| Eccentricity: | 0.0004293 |
| inclination: | 70.9996° |
| perigee height: | 841 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 224.6701° |
| argument of perigee: | 3.8877° |
| revolutions per day: | 14.14596418 |
| mean anomaly at epoch: | 356.2278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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