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 68498U 26145.39310382 +.00000000 +00000-0 +11608-3 0 00004
2 68498 97.7534 103.9305 0003921 117.7457 242.4159 14.91392047 07
| Epoch (UTC): | 25 May 2026 09:26:04 |
| Eccentricity: | 0.0003921 |
| inclination: | 97.7534° |
| perigee height: | 591 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 103.9305° |
| argument of perigee: | 117.7457° |
| revolutions per day: | 14.91392047 |
| mean anomaly at epoch: | 242.4159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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