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 49263U 26145.25812031 +.00000000 +00000-0 +12615-2 0 00004
2 49263 97.4191 242.4981 0003765 263.1184 96.9656 15.81807184 07
| Epoch (UTC): | 25 May 2026 06:11:41 |
| Eccentricity: | 0.0003765 |
| inclination: | 97.4191° |
| perigee height: | 323 km |
| apogee height: | 328 km |
| right ascension of ascending node: | 242.4981° |
| argument of perigee: | 263.1184° |
| revolutions per day: | 15.81807184 |
| mean anomaly at epoch: | 96.9656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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