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 60113U 26145.44061476 +.00000000 +00000-0 +32631-5 0 00004
2 60113 53.1586 203.2225 0001034 76.5922 283.5211 15.69696531 09
| Epoch (UTC): | 25 May 2026 10:34:29 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 203.2225° |
| argument of perigee: | 76.5922° |
| revolutions per day: | 15.69696531 |
| mean anomaly at epoch: | 283.5211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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