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 63260U 26145.45687213 +.00000000 +00000-0 +14837-3 0 00000
2 63260 97.6876 37.3146 0003072 68.6343 291.5205 14.94598576 00
| Epoch (UTC): | 25 May 2026 10:57:53 |
| Eccentricity: | 0.0003072 |
| inclination: | 97.6876° |
| perigee height: | 581 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 37.3146° |
| argument of perigee: | 68.6343° |
| revolutions per day: | 14.94598576 |
| mean anomaly at epoch: | 291.5205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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