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 63798U 26145.53083560 +.00000000 +00000-0 +54275-3 0 00000
2 63798 43.0001 338.6052 0000922 310.4745 49.6026 15.27597688 02
| Epoch (UTC): | 25 May 2026 12:44:24 |
| Eccentricity: | 0.0000922 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.6052° |
| argument of perigee: | 310.4745° |
| revolutions per day: | 15.27597688 |
| mean anomaly at epoch: | 49.6026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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