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 65258U 26145.35569315 +.00000000 +00000-0 +32349-3 0 00008
2 65258 97.4459 188.1514 0001270 141.3741 218.7577 15.05658080 00
| Epoch (UTC): | 25 May 2026 08:32:11 |
| Eccentricity: | 0.0001270 |
| inclination: | 97.4459° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 188.1514° |
| argument of perigee: | 141.3741° |
| revolutions per day: | 15.05658080 |
| mean anomaly at epoch: | 218.7577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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