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 49102U 26145.24411156 +.00000000 +00000-0 +19041-3 0 00009
2 49102 87.9160 340.0237 0001889 89.8970 270.2379 13.18685654 02
| Epoch (UTC): | 25 May 2026 05:51:31 |
| Eccentricity: | 0.0001889 |
| inclination: | 87.9160° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0237° |
| argument of perigee: | 89.8970° |
| revolutions per day: | 13.18685654 |
| mean anomaly at epoch: | 270.2379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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