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 68248U 26145.12765213 +.00000000 +00000-0 +60394-3 0 00001
2 68248 53.1573 301.9488 0000777 56.5862 303.5213 15.30217546 01
| Epoch (UTC): | 25 May 2026 03:03:49 |
| Eccentricity: | 0.0000777 |
| inclination: | 53.1573° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 301.9488° |
| argument of perigee: | 56.5862° |
| revolutions per day: | 15.30217546 |
| mean anomaly at epoch: | 303.5213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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