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 49148U 26145.54619120 +.00000000 +00000-0 -56854-4 0 00008
2 49148 70.0000 81.6906 0003231 265.3683 94.7106 14.97513729 02
| Epoch (UTC): | 25 May 2026 13:06:30 |
| Eccentricity: | 0.0003231 |
| inclination: | 70.0000° |
| perigee height: | 572 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 81.6906° |
| argument of perigee: | 265.3683° |
| revolutions per day: | 14.97513729 |
| mean anomaly at epoch: | 94.7106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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