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 60996U 26145.35732292 +.00000000 +00000-0 +14633-4 0 00005
2 60996 53.1601 263.5009 0000783 68.2193 291.8908 15.69715674 08
| Epoch (UTC): | 25 May 2026 08:34:32 |
| Eccentricity: | 0.0000783 |
| inclination: | 53.1601° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 263.5009° |
| argument of perigee: | 68.2193° |
| revolutions per day: | 15.69715674 |
| mean anomaly at epoch: | 291.8908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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