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 49397U 26145.36280170 +.00000000 +00000-0 +27858-3 0 00003
2 49397 97.3271 178.9861 0008830 17.2250 342.9284 15.21195612 04
| Epoch (UTC): | 25 May 2026 08:42:26 |
| Eccentricity: | 0.0008830 |
| inclination: | 97.3271° |
| perigee height: | 496 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 178.9861° |
| argument of perigee: | 17.2250° |
| revolutions per day: | 15.21195612 |
| mean anomaly at epoch: | 342.9284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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