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 49087U 26145.56313417 +.00000000 +00000-0 +26770-4 0 00005
2 49087 87.9155 10.3669 0001973 83.9669 276.1687 13.17647171 06
| Epoch (UTC): | 25 May 2026 13:30:54 |
| Eccentricity: | 0.0001973 |
| inclination: | 87.9155° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3669° |
| argument of perigee: | 83.9669° |
| revolutions per day: | 13.17647171 |
| mean anomaly at epoch: | 276.1687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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