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 26156.06954730 +.00000000 +00000-0 -40409-4 0 00000
2 28353 71.0024 49.1200 0007472 268.4538 91.5729 14.14613082 02
| Epoch (UTC): | 05 June 2026 01:40:08 |
| Eccentricity: | 0.0007472 |
| inclination: | 71.0024° |
| perigee height: | 838 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 49.1200° |
| argument of perigee: | 268.4538° |
| revolutions per day: | 14.14613082 |
| mean anomaly at epoch: | 91.5729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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