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 63699U 26145.49404434 +.00000000 +00000-0 +60970-3 0 00001
2 63699 53.1580 223.1698 0000925 60.4356 299.6737 15.30213465 01
| Epoch (UTC): | 25 May 2026 11:51:25 |
| Eccentricity: | 0.0000925 |
| inclination: | 53.1580° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.1698° |
| argument of perigee: | 60.4356° |
| revolutions per day: | 15.30213465 |
| mean anomaly at epoch: | 299.6737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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