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 49313U 26145.64068478 +.00000000 +00000-0 +33483-3 0 00008
2 49313 87.9166 278.9503 0002236 104.3003 255.8379 13.20772641 09
| Epoch (UTC): | 25 May 2026 15:22:35 |
| Eccentricity: | 0.0002236 |
| inclination: | 87.9166° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9503° |
| argument of perigee: | 104.3003° |
| revolutions per day: | 13.20772641 |
| mean anomaly at epoch: | 255.8379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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