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 68453U 26145.33057123 +.00000000 +00000-0 +33324-3 0 00009
2 68453 97.4536 104.1485 0004321 95.9494 264.2233 15.18436924 00
| Epoch (UTC): | 25 May 2026 07:56:01 |
| Eccentricity: | 0.0004321 |
| inclination: | 97.4536° |
| perigee height: | 508 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 104.1485° |
| argument of perigee: | 95.9494° |
| revolutions per day: | 15.18436924 |
| mean anomaly at epoch: | 264.2233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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