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 68242U 26145.44156966 +.00000000 +00000-0 +66368-3 0 00006
2 68242 53.1603 300.3659 0001134 61.3048 298.8066 15.30210124 07
| Epoch (UTC): | 25 May 2026 10:35:51 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.3659° |
| argument of perigee: | 61.3048° |
| revolutions per day: | 15.30210124 |
| mean anomaly at epoch: | 298.8066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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