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 53417U 26145.26106796 +.00000000 +00000-0 +25078-3 0 00003
2 53417 53.2154 130.3773 0001443 77.2896 282.8258 15.08844489 03
| Epoch (UTC): | 25 May 2026 06:15:56 |
| Eccentricity: | 0.0001443 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 130.3773° |
| argument of perigee: | 77.2896° |
| revolutions per day: | 15.08844489 |
| mean anomaly at epoch: | 282.8258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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