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 53141U 26145.41747521 +.00000000 +00000-0 +30832-5 0 00007
2 53141 53.2101 189.6777 0000968 89.6666 270.4438 15.08851871 09
| Epoch (UTC): | 25 May 2026 10:01:09 |
| Eccentricity: | 0.0000968 |
| inclination: | 53.2101° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 189.6777° |
| argument of perigee: | 89.6666° |
| revolutions per day: | 15.08851871 |
| mean anomaly at epoch: | 270.4438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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