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 63414U 26145.38435618 +.00000000 +00000-0 +50687-3 0 00006
2 63414 43.0016 34.3908 0000995 268.2192 91.8546 15.27600882 06
| Epoch (UTC): | 25 May 2026 09:13:28 |
| Eccentricity: | 0.0000995 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 34.3908° |
| argument of perigee: | 268.2192° |
| revolutions per day: | 15.27600882 |
| mean anomaly at epoch: | 91.8546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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