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 49338U 26145.60234733 +.00000000 +00000-0 +19468-3 0 00007
2 49338 97.6671 271.8667 0017242 306.8723 53.0923 15.07572051 02
| Epoch (UTC): | 25 May 2026 14:27:22 |
| Eccentricity: | 0.0017242 |
| inclination: | 97.6671° |
| perigee height: | 532 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 271.8667° |
| argument of perigee: | 306.8723° |
| revolutions per day: | 15.07572051 |
| mean anomaly at epoch: | 53.0923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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