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 26141.21330273 +.00000000 +00000-0 +10460-3 0 00005
2 53807 53.2273 160.5704 0007432 89.6740 270.5117 15.37895607 04
| Epoch (UTC): | 21 May 2026 05:07:09 |
| Eccentricity: | 0.0007432 |
| inclination: | 53.2273° |
| perigee height: | 447 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 160.5704° |
| argument of perigee: | 89.6740° |
| revolutions per day: | 15.37895607 |
| mean anomaly at epoch: | 270.5117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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