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 60399U 26145.21157470 +.00000000 +00000-0 +20698-4 0 00004
2 60399 53.1583 68.8811 0000787 70.1594 289.9508 15.69706558 07
| Epoch (UTC): | 25 May 2026 05:04:40 |
| Eccentricity: | 0.0000787 |
| inclination: | 53.1583° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 68.8811° |
| argument of perigee: | 70.1594° |
| revolutions per day: | 15.69706558 |
| mean anomaly at epoch: | 289.9508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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