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 49262U 26145.16047853 +.00000000 +00000-0 +42675-3 0 00005
2 49262 97.3830 210.8096 0010766 158.0515 202.1192 15.35564692 09
| Epoch (UTC): | 25 May 2026 03:51:05 |
| Eccentricity: | 0.0010766 |
| inclination: | 97.3830° |
| perigee height: | 452 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 210.8096° |
| argument of perigee: | 158.0515° |
| revolutions per day: | 15.35564692 |
| mean anomaly at epoch: | 202.1192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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