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 49104U 26145.24073674 +.00000000 +00000-0 +29618-3 0 00001
2 49104 87.9168 340.0238 0002086 90.1840 269.9531 13.18686068 09
| Epoch (UTC): | 25 May 2026 05:46:39 |
| Eccentricity: | 0.0002086 |
| inclination: | 87.9168° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0238° |
| argument of perigee: | 90.1840° |
| revolutions per day: | 13.18686068 |
| mean anomaly at epoch: | 269.9531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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