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 60149U 26145.21874553 +.00000000 +00000-0 +10477-4 0 00009
2 60149 53.1620 324.4148 0001179 92.8489 267.2647 15.30191366 02
| Epoch (UTC): | 25 May 2026 05:14:59 |
| Eccentricity: | 0.0001179 |
| inclination: | 53.1620° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 324.4148° |
| argument of perigee: | 92.8489° |
| revolutions per day: | 15.30191366 |
| mean anomaly at epoch: | 267.2647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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