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 63739U 26145.20010083 +.00000000 +00000-0 +12714-3 0 00001
2 63739 51.9028 122.2854 0000680 57.3263 302.7765 14.79923570 06
| Epoch (UTC): | 25 May 2026 04:48:08 |
| Eccentricity: | 0.0000680 |
| inclination: | 51.9028° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 122.2854° |
| argument of perigee: | 57.3263° |
| revolutions per day: | 14.79923570 |
| mean anomaly at epoch: | 302.7765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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