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 55844U 26145.52741323 +.00000000 +00000-0 +24727-3 0 00009
2 55844 97.3538 221.3818 0003329 122.5403 237.6157 15.23505160 01
| Epoch (UTC): | 25 May 2026 12:39:28 |
| Eccentricity: | 0.0003329 |
| inclination: | 97.3538° |
| perigee height: | 493 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 221.3818° |
| argument of perigee: | 122.5403° |
| revolutions per day: | 15.23505160 |
| mean anomaly at epoch: | 237.6157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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