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 49195U 26145.23919166 +.00000000 +00000-0 +18056-4 0 00000
2 49195 87.9168 340.0225 0002118 88.6239 271.5136 13.18685057 02
| Epoch (UTC): | 25 May 2026 05:44:26 |
| Eccentricity: | 0.0002118 |
| inclination: | 87.9168° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0225° |
| argument of perigee: | 88.6239° |
| revolutions per day: | 13.18685057 |
| mean anomaly at epoch: | 271.5136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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