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 49178U 26145.32523323 +.00000000 +00000-0 -48212-3 0 00004
2 49178 69.9995 101.2189 0003193 265.9348 94.1446 14.98288215 09
| Epoch (UTC): | 25 May 2026 07:48:20 |
| Eccentricity: | 0.0003193 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 101.2189° |
| argument of perigee: | 265.9348° |
| revolutions per day: | 14.98288215 |
| mean anomaly at epoch: | 94.1446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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