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 60494U 26145.21213777 +.00000000 +00000-0 +37706-3 0 00000
2 60494 97.3732 228.5693 0003013 20.2288 339.9077 15.40374937 01
| Epoch (UTC): | 25 May 2026 05:05:28 |
| Eccentricity: | 0.0003013 |
| inclination: | 97.3732° |
| perigee height: | 443 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 228.5693° |
| argument of perigee: | 20.2288° |
| revolutions per day: | 15.40374937 |
| mean anomaly at epoch: | 339.9077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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