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 68495U 26145.58335647 +.00000000 +00000-0 -73253-2 0 00007
2 68495 97.7597 103.1254 0004128 84.0816 301.1282 14.59512452 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0004128 |
| inclination: | 97.7597° |
| perigee height: | 692 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 103.1254° |
| argument of perigee: | 84.0816° |
| revolutions per day: | 14.59512452 |
| mean anomaly at epoch: | 301.1282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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