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 63150U 26145.46101176 +.00000000 +00000-0 +68657-3 0 00007
2 63150 42.9989 302.6543 0001179 272.2436 87.8281 15.27600193 03
| Epoch (UTC): | 25 May 2026 11:03:51 |
| Eccentricity: | 0.0001179 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.6543° |
| argument of perigee: | 272.2436° |
| revolutions per day: | 15.27600193 |
| mean anomaly at epoch: | 87.8281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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