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 58449U 26145.46222941 +.00000000 +00000-0 +11226-3 0 00006
2 58449 43.0008 302.1840 0001510 281.6745 78.3937 15.27573583 08
| Epoch (UTC): | 25 May 2026 11:05:36 |
| Eccentricity: | 0.0001510 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.1840° |
| argument of perigee: | 281.6745° |
| revolutions per day: | 15.27573583 |
| mean anomaly at epoch: | 78.3937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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