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 63970U 26145.27303691 +.00000000 +00000-0 +60967-3 0 00008
2 63970 43.0029 103.2852 0002120 260.2346 99.8266 15.27592140 00
| Epoch (UTC): | 25 May 2026 06:33:10 |
| Eccentricity: | 0.0002120 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.2852° |
| argument of perigee: | 260.2346° |
| revolutions per day: | 15.27592140 |
| mean anomaly at epoch: | 99.8266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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