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 49159U 26145.32937150 +.00000000 +00000-0 -84386-4 0 00003
2 49159 69.9995 101.2215 0003310 272.3212 87.7568 14.98324028 07
| Epoch (UTC): | 25 May 2026 07:54:17 |
| Eccentricity: | 0.0003310 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 101.2215° |
| argument of perigee: | 272.3212° |
| revolutions per day: | 14.98324028 |
| mean anomaly at epoch: | 87.7568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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