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 55339U 26145.53627663 +.00000000 +00000-0 -87349-5 0 00001
2 55339 43.0022 233.0389 0000998 272.9774 87.0964 15.27576232 04
| Epoch (UTC): | 25 May 2026 12:52:14 |
| Eccentricity: | 0.0000998 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 233.0389° |
| argument of perigee: | 272.9774° |
| revolutions per day: | 15.27576232 |
| mean anomaly at epoch: | 87.0964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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