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 60049U 26145.28011068 +.00000000 +00000-0 +37262-4 0 00000
2 60049 53.1610 248.4658 0000270 38.5075 321.5962 15.69724868 05
| Epoch (UTC): | 25 May 2026 06:43:21 |
| Eccentricity: | 0.0000270 |
| inclination: | 53.1610° |
| perigee height: | 360 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 248.4658° |
| argument of perigee: | 38.5075° |
| revolutions per day: | 15.69724868 |
| mean anomaly at epoch: | 321.5962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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