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 26156.98880058 +.00000000 +00000-0 -52859-4 0 00004
2 28353 71.0024 47.1911 0007476 267.5401 92.4865 14.14612943 08
| Epoch (UTC): | 05 June 2026 23:43:52 |
| Eccentricity: | 0.0007476 |
| inclination: | 71.0024° |
| perigee height: | 838 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 47.1911° |
| argument of perigee: | 267.5401° |
| revolutions per day: | 14.14612943 |
| mean anomaly at epoch: | 92.4865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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