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 63834U 26145.14089750 +.00000000 +00000-0 +33835-3 0 00004
2 63834 97.3998 39.7311 0003273 202.2889 157.8209 15.27913102 04
| Epoch (UTC): | 25 May 2026 03:22:53 |
| Eccentricity: | 0.0003273 |
| inclination: | 97.3998° |
| perigee height: | 480 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 39.7311° |
| argument of perigee: | 202.2889° |
| revolutions per day: | 15.27913102 |
| mean anomaly at epoch: | 157.8209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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