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 60138U 26145.66668980 +.00000000 +00000-0 -73601-3 0 00009
2 60138 53.1586 322.1182 0001267 91.5662 327.9993 15.30207566 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001267 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 322.1182° |
| argument of perigee: | 91.5662° |
| revolutions per day: | 15.30207566 |
| mean anomaly at epoch: | 327.9993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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