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 33498U 26039.06338453 +.00000000 +00000-0 +53455-3 0 00007
2 33498 98.1437 341.3114 0006930 229.4601 130.6016 14.94621532 04
| Epoch (UTC): | 08 February 2026 01:31:16 |
| Eccentricity: | 0.0006930 |
| inclination: | 98.1437° |
| perigee height: | 579 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 341.3114° |
| argument of perigee: | 229.4601° |
| revolutions per day: | 14.94621532 |
| mean anomaly at epoch: | 130.6016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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