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 49383U 26145.61887800 +.00000000 +00000-0 +13103-3 0 00007
2 49383 98.2440 279.4024 0000279 48.0258 312.0968 14.64171686 02
| Epoch (UTC): | 25 May 2026 14:51:11 |
| Eccentricity: | 0.0000279 |
| inclination: | 98.2440° |
| perigee height: | 680 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 279.4024° |
| argument of perigee: | 48.0258° |
| revolutions per day: | 14.64171686 |
| mean anomaly at epoch: | 312.0968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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