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 49088U 26145.33687609 +.00000000 +00000-0 -31293-4 0 00005
2 49088 87.9163 10.3898 0001936 87.7028 272.4325 13.17649704 02
| Epoch (UTC): | 25 May 2026 08:05:06 |
| Eccentricity: | 0.0001936 |
| inclination: | 87.9163° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3898° |
| argument of perigee: | 87.7028° |
| revolutions per day: | 13.17649704 |
| mean anomaly at epoch: | 272.4325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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