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 49165U 26145.31267712 +.00000000 +00000-0 +27908-4 0 00005
2 49165 69.9993 101.2767 0003333 268.8426 91.2352 14.98334266 02
| Epoch (UTC): | 25 May 2026 07:30:15 |
| Eccentricity: | 0.0003333 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 101.2767° |
| argument of perigee: | 268.8426° |
| revolutions per day: | 14.98334266 |
| mean anomaly at epoch: | 91.2352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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