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 60098U 26145.41387670 +.00000000 +00000-0 +15050-5 0 00006
2 60098 53.1615 40.7202 0001099 101.7030 258.4095 15.30189919 01
| Epoch (UTC): | 25 May 2026 09:55:58 |
| Eccentricity: | 0.0001099 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.7202° |
| argument of perigee: | 101.7030° |
| revolutions per day: | 15.30189919 |
| mean anomaly at epoch: | 258.4095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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