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 53807U 26156.09445001 +.00000000 +00000-0 +19133-3 0 00009
2 53807 53.2291 90.7369 0007068 127.5569 232.6079 15.38113643 01
| Epoch (UTC): | 05 June 2026 02:16:00 |
| Eccentricity: | 0.0007068 |
| inclination: | 53.2291° |
| perigee height: | 447 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 90.7369° |
| argument of perigee: | 127.5569° |
| revolutions per day: | 15.38113643 |
| mean anomaly at epoch: | 232.6079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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