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 68201U 26145.16247353 +.00000000 +00000-0 +31622-3 0 00006
2 68201 97.5343 220.3399 0012281 35.0953 325.1084 15.11103765 00
| Epoch (UTC): | 25 May 2026 03:53:57 |
| Eccentricity: | 0.0012281 |
| inclination: | 97.5343° |
| perigee height: | 524 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 220.3399° |
| argument of perigee: | 35.0953° |
| revolutions per day: | 15.11103765 |
| mean anomaly at epoch: | 325.1084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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