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 63148U 26145.45715969 +.00000000 +00000-0 +63762-3 0 00006
2 63148 43.0018 302.6323 0001045 267.5121 92.5611 15.27592718 04
| Epoch (UTC): | 25 May 2026 10:58:18 |
| Eccentricity: | 0.0001045 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.6323° |
| argument of perigee: | 267.5121° |
| revolutions per day: | 15.27592718 |
| mean anomaly at epoch: | 92.5611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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