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 60041U 26145.31446024 +.00000000 +00000-0 +81148-5 0 00003
2 60041 53.1580 248.6955 0001038 76.5568 283.5565 15.69729806 00
| Epoch (UTC): | 25 May 2026 07:32:49 |
| Eccentricity: | 0.0001038 |
| inclination: | 53.1580° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 248.6955° |
| argument of perigee: | 76.5568° |
| revolutions per day: | 15.69729806 |
| mean anomaly at epoch: | 283.5565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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