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 41884U 26152.01467613 +.00000000 +00000-0 +36731-3 0 00005
2 41884 34.9584 7.6220 0008155 348.9921 11.0624 15.55898469 06
| Epoch (UTC): | 01 June 2026 00:21:08 |
| Eccentricity: | 0.0008155 |
| inclination: | 34.9584° |
| perigee height: | 394 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 7.6220° |
| argument of perigee: | 348.9921° |
| revolutions per day: | 15.55898469 |
| mean anomaly at epoch: | 11.0624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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