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 61243U 26145.14057612 +.00000000 +00000-0 +28537-4 0 00002
2 61243 53.1591 39.4142 0000649 107.4619 252.6470 15.69724131 07
| Epoch (UTC): | 25 May 2026 03:22:25 |
| Eccentricity: | 0.0000649 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 39.4142° |
| argument of perigee: | 107.4619° |
| revolutions per day: | 15.69724131 |
| mean anomaly at epoch: | 252.6470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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