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 60045U 26145.54952198 +.00000000 +00000-0 -50532-4 0 00009
2 60045 53.1586 247.3074 0001588 97.6628 262.4570 15.69707026 01
| Epoch (UTC): | 25 May 2026 13:11:18 |
| Eccentricity: | 0.0001588 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 247.3074° |
| argument of perigee: | 97.6628° |
| revolutions per day: | 15.69707026 |
| mean anomaly at epoch: | 262.4570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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