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 61527U 26145.27153233 +.00000000 +00000-0 +36415-4 0 00001
2 61527 53.1603 146.9907 0001419 86.4267 273.6896 15.30192497 07
| Epoch (UTC): | 25 May 2026 06:31:00 |
| Eccentricity: | 0.0001419 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.9907° |
| argument of perigee: | 86.4267° |
| revolutions per day: | 15.30192497 |
| mean anomaly at epoch: | 273.6896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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