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 49132U 26145.61309091 +.00000000 +00000-0 -20166-4 0 00009
2 49132 69.9994 100.3786 0003453 262.2395 97.8372 14.98331527 05
| Epoch (UTC): | 25 May 2026 14:42:51 |
| Eccentricity: | 0.0003453 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 100.3786° |
| argument of perigee: | 262.2395° |
| revolutions per day: | 14.98331527 |
| mean anomaly at epoch: | 97.8372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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