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 52276U 26145.24497016 +.00000000 +00000-0 -17403-3 0 00005
2 52276 53.2143 125.4485 0001174 79.6907 280.4218 15.08852029 07
| Epoch (UTC): | 25 May 2026 05:52:45 |
| Eccentricity: | 0.0001174 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 125.4485° |
| argument of perigee: | 79.6907° |
| revolutions per day: | 15.08852029 |
| mean anomaly at epoch: | 280.4218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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