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 02498U 26136.32286560 +.00000000 +00000-0 +91550-4 0 00000
2 02498 40.6266 235.7368 2067822 347.6577 8.0028 10.56406618 04
| Epoch (UTC): | 16 May 2026 07:44:55 |
| Eccentricity: | 0.2067822 |
| inclination: | 40.6266° |
| perigee height: | 581 km |
| apogee height: | 4210 km |
| right ascension of ascending node: | 235.7368° |
| argument of perigee: | 347.6577° |
| revolutions per day: | 10.56406618 |
| mean anomaly at epoch: | 8.0028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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