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 53412U 26145.33834668 +.00000000 +00000-0 -24613-6 0 00000
2 53412 53.2130 130.0335 0001149 84.6688 275.4436 15.08843628 07
| Epoch (UTC): | 25 May 2026 08:07:13 |
| Eccentricity: | 0.0001149 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 130.0335° |
| argument of perigee: | 84.6688° |
| revolutions per day: | 15.08843628 |
| mean anomaly at epoch: | 275.4436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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