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 63272U 26145.33659987 +.00000000 +00000-0 +16076-2 0 00003
2 63272 42.9991 10.2665 0001515 61.8521 298.2499 15.70894668 08
| Epoch (UTC): | 25 May 2026 08:04:42 |
| Eccentricity: | 0.0001515 |
| inclination: | 42.9991° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 10.2665° |
| argument of perigee: | 61.8521° |
| revolutions per day: | 15.70894668 |
| mean anomaly at epoch: | 298.2499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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