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 49138U 26145.28764368 +.00000000 +00000-0 +47087-4 0 00000
2 49138 69.9992 101.3319 0003864 268.3827 91.6889 14.98339384 09
| Epoch (UTC): | 25 May 2026 06:54:12 |
| Eccentricity: | 0.0003864 |
| inclination: | 69.9992° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 101.3319° |
| argument of perigee: | 268.3827° |
| revolutions per day: | 14.98339384 |
| mean anomaly at epoch: | 91.6889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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