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 59449U 26145.05360381 +.00000000 +00000-0 +10229-3 0 00005
2 59449 45.6093 37.1704 0003444 294.2132 65.8389 14.99022004 00
| Epoch (UTC): | 25 May 2026 01:17:11 |
| Eccentricity: | 0.0003444 |
| inclination: | 45.6093° |
| perigee height: | 568 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 37.1704° |
| argument of perigee: | 294.2132° |
| revolutions per day: | 14.99022004 |
| mean anomaly at epoch: | 65.8389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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