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 49196U 26145.46653816 +.00000000 +00000-0 +14149-3 0 00001
2 49196 87.9161 339.9833 0002214 85.3325 274.8059 13.18686276 09
| Epoch (UTC): | 25 May 2026 11:11:48 |
| Eccentricity: | 0.0002214 |
| inclination: | 87.9161° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9833° |
| argument of perigee: | 85.3325° |
| revolutions per day: | 13.18686276 |
| mean anomaly at epoch: | 274.8059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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