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 53280U 26145.31576902 +.00000000 +00000-0 +14953-4 0 00008
2 53280 53.2124 154.8076 0001532 89.4943 270.6225 15.08835720 09
| Epoch (UTC): | 25 May 2026 07:34:42 |
| Eccentricity: | 0.0001532 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.8076° |
| argument of perigee: | 89.4943° |
| revolutions per day: | 15.08835720 |
| mean anomaly at epoch: | 270.6225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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