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 63700U 26145.38968655 +.00000000 +00000-0 +54202-3 0 00003
2 63700 53.1587 223.2248 0001330 113.6034 246.5107 15.30208630 08
| Epoch (UTC): | 25 May 2026 09:21:08 |
| Eccentricity: | 0.0001330 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.2248° |
| argument of perigee: | 113.6034° |
| revolutions per day: | 15.30208630 |
| mean anomaly at epoch: | 246.5107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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