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 data is extracted from the following two-line orbital elements,
1 00704U 63049B 25341.22780359 .00000117 00000-0 17624-3 0 9996
2 00704 89.9229 71.9821 0036418 129.6685 258.7617 13.47102836 45481
| Epoch (UTC): | 07 December 2025 05:28:02 |
| Eccentricity: | 0.0036418 |
| inclination: | 89.9229° |
| perigee height: | 1056 km |
| apogee height: | 1110 km |
| right ascension of ascending node: | 71.9821° |
| argument of perigee: | 129.6685° |
| revolutions per day: | 13.47102836 |
| mean anomaly at epoch: | 258.7617° |
| orbit number at epoch: | 4548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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