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 60351U 26145.12012927 +.00000000 +00000-0 -43657-4 0 00000
2 60351 53.1617 79.4276 0001377 103.5489 256.5667 15.34375025 05
| Epoch (UTC): | 25 May 2026 02:52:59 |
| Eccentricity: | 0.0001377 |
| inclination: | 53.1617° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 79.4276° |
| argument of perigee: | 103.5489° |
| revolutions per day: | 15.34375025 |
| mean anomaly at epoch: | 256.5667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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