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 55140U 26145.32841859 +.00000000 +00000-0 +11511-3 0 00008
2 55140 87.9153 10.4107 0002001 93.3803 266.7557 13.17651748 03
| Epoch (UTC): | 25 May 2026 07:52:55 |
| Eccentricity: | 0.0002001 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4107° |
| argument of perigee: | 93.3803° |
| revolutions per day: | 13.17651748 |
| mean anomaly at epoch: | 266.7557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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