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 60949U 26145.63934031 +.00000000 +00000-0 +53857-3 0 00009
2 60949 34.9966 339.9859 0001025 220.7836 139.2802 15.23029684 04
| Epoch (UTC): | 25 May 2026 15:20:39 |
| Eccentricity: | 0.0001025 |
| inclination: | 34.9966° |
| perigee height: | 496 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 339.9859° |
| argument of perigee: | 220.7836° |
| revolutions per day: | 15.23029684 |
| mean anomaly at epoch: | 139.2802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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