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 49188U 26145.30312557 +.00000000 +00000-0 +28194-3 0 00004
2 49188 87.9169 339.9980 0001593 88.0144 272.1171 13.18686279 08
| Epoch (UTC): | 25 May 2026 07:16:30 |
| Eccentricity: | 0.0001593 |
| inclination: | 87.9169° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9980° |
| argument of perigee: | 88.0144° |
| revolutions per day: | 13.18686279 |
| mean anomaly at epoch: | 272.1171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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