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 60341U 26145.09424484 +.00000000 +00000-0 +18324-4 0 00002
2 60341 53.1605 80.6840 0001343 81.2641 278.8511 15.30195638 08
| Epoch (UTC): | 25 May 2026 02:15:42 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.6840° |
| argument of perigee: | 81.2641° |
| revolutions per day: | 15.30195638 |
| mean anomaly at epoch: | 278.8511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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