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 53168U 26145.52879094 +.00000000 +00000-0 +36108-4 0 00000
2 53168 53.2107 179.1759 0000940 84.4541 275.6558 15.08835157 02
| Epoch (UTC): | 25 May 2026 12:41:27 |
| Eccentricity: | 0.0000940 |
| inclination: | 53.2107° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 179.1759° |
| argument of perigee: | 84.4541° |
| revolutions per day: | 15.08835157 |
| mean anomaly at epoch: | 275.6558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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