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 53488U 26145.32640659 +.00000000 +00000-0 -57752-4 0 00005
2 53488 97.4455 266.4387 0002484 107.1407 253.0092 15.05640970 06
| Epoch (UTC): | 25 May 2026 07:50:01 |
| Eccentricity: | 0.0002484 |
| inclination: | 97.4455° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 266.4387° |
| argument of perigee: | 107.1407° |
| revolutions per day: | 15.05640970 |
| mean anomaly at epoch: | 253.0092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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