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 49744U 26145.46671179 +.00000000 +00000-0 +17084-3 0 00003
2 49744 53.2118 164.3476 0000989 75.0079 285.1023 15.08827702 06
| Epoch (UTC): | 25 May 2026 11:12:03 |
| Eccentricity: | 0.0000989 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.3476° |
| argument of perigee: | 75.0079° |
| revolutions per day: | 15.08827702 |
| mean anomaly at epoch: | 285.1023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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