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 55492U 26145.38219490 +.00000000 +00000-0 -10118-5 0 00009
2 55492 43.0036 266.6641 0001205 273.9940 86.0774 15.27576342 00
| Epoch (UTC): | 25 May 2026 09:10:21 |
| Eccentricity: | 0.0001205 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.6641° |
| argument of perigee: | 273.9940° |
| revolutions per day: | 15.27576342 |
| mean anomaly at epoch: | 86.0774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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