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 16624U 26146.27530640 +.00000000 +00000-0 +30049-3 0 00007
2 16624 63.2982 175.9755 0795401 115.8608 252.6626 13.71886198 06
| Epoch (UTC): | 26 May 2026 06:36:26 |
| Eccentricity: | 0.0795401 |
| inclination: | 63.2982° |
| perigee height: | 407 km |
| apogee height: | 1579 km |
| right ascension of ascending node: | 175.9755° |
| argument of perigee: | 115.8608° |
| revolutions per day: | 13.71886198 |
| mean anomaly at epoch: | 252.6626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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