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 63307U 26145.32247203 +.00000000 +00000-0 +16349-2 0 00008
2 63307 42.9987 162.2850 0001432 258.0340 102.0368 15.70948011 02
| Epoch (UTC): | 25 May 2026 07:44:21 |
| Eccentricity: | 0.0001432 |
| inclination: | 42.9987° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 162.2850° |
| argument of perigee: | 258.0340° |
| revolutions per day: | 15.70948011 |
| mean anomaly at epoch: | 102.0368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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