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 49316U 26145.58920610 +.00000000 +00000-0 +93201-4 0 00004
2 49316 97.4484 333.5101 0014767 116.5697 243.7052 15.18418437 02
| Epoch (UTC): | 25 May 2026 14:08:27 |
| Eccentricity: | 0.0014767 |
| inclination: | 97.4484° |
| perigee height: | 500 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 333.5101° |
| argument of perigee: | 116.5697° |
| revolutions per day: | 15.18418437 |
| mean anomaly at epoch: | 243.7052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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