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EZIE-C

In orbit NORAD 63249 PDCU-2422-0291-6540-9954

Falcon 9

Carrier rocket

База Вандерберг

Spaceport

0

Observations all time

Mission information
Spacecraft name
EZIE-C
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9
Spaceport
База Вандерберг
Launch time
2025-03-15 06:43:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
568.26 km
Apogee
572.02 km
Inclination
97.7°
Period
96.1 min
Semi-major axis
6948.3 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-09 12:46:41 UTC
Two-line elements (TLE)
1 63249U 25052AR  26282.15667231  .00002725  00000-0  23583-3 0  9999
2 63249 97.6702 172.3088 0002707 171.8214 188.3053 14.97981446 85729
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-10 17:34:44 EZIE-C
NORAD 63249
COSMOS 249 DEB
NORAD 3790
4.806 15.08 7.4e-08
2026-10-11 04:35:36 EZIE-C
NORAD 63249
STARLINK-36224
NORAD 67203
3.239 15.06 4.4e-06
2026-10-11 09:34:32 STARLINK-5508
NORAD 55639
EZIE-C
NORAD 63249
4.392 15.03 2.4e-06
2026-10-11 10:22:30 STARLINK-5494
NORAD 55650
EZIE-C
NORAD 63249
3.965 15.04 3.0e-06
2026-10-11 17:57:49 EZIE-C
NORAD 63249
ION SCV-018
NORAD 64575
1.890 13.89 6.2e-07
2026-10-12 01:22:56 EZIE-C
NORAD 63249
STARLINK-36182
NORAD 67192
2.268 15.04 9.1e-06
2026-10-12 02:58:57 EZIE-C
NORAD 63249
STARLINK-36173
NORAD 67210
4.175 15.04 2.7e-06
2026-10-12 15:33:46 EZIE-C
NORAD 63249
PEGASUS DEB
NORAD 24996
3.973 10.19 2.2e-07
2026-10-12 18:53:24 STARLINK-5423
NORAD 55670
EZIE-C
NORAD 63249
2.290 14.87 9.7e-06
2026-10-13 06:10:55 EZIE-C
NORAD 63249
STARLINK-36211
NORAD 67218
3.300 15.01 4.4e-06
2026-10-13 07:46:57 EZIE-C
NORAD 63249
STARLINK-36279
NORAD 67193
4.537 15.00 2.3e-06
2026-10-13 13:46:49 EZIE-C
NORAD 63249
STARLINK-35838
NORAD 66836
2.194 5.38 2.6e-05
2026-10-13 14:34:53 EZIE-C
NORAD 63249
STARLINK-35838
NORAD 66836
4.756 5.39 5.6e-06
2026-10-14 07:41:16 STARLINK-5640
NORAD 55436
EZIE-C
NORAD 63249
4.897 11.44 3.9e-06
2026-10-14 08:38:06 EZIE-C
NORAD 63249
CZ-6A DEB
NORAD 54484
1.352 14.90 9.0e-07
2026-10-15 03:00:38 EZIE-C
NORAD 63249
STARLINK-36280
NORAD 67211
3.266 14.91 4.7e-06
2026-10-15 04:36:44 EZIE-C
NORAD 63249
STARLINK-36270
NORAD 67200
2.225 14.90 1.0e-05
2026-10-15 10:31:55 EZIE-C
NORAD 63249
3CAT-4
NORAD 60236
3.712 4.86 3.1e-07
2026-10-15 17:21:04 EZIE-C
NORAD 63249
STARLINK-34675
NORAD 64809
2.040 13.23 1.8e-05
2026-10-16 03:38:26 EZIE-C
NORAD 63249
FENGYUN 1C DEB
NORAD 31878
1.828 11.29 9.4e-07
2026-10-16 04:37:32 STARLINK-5276
NORAD 55399
EZIE-C
NORAD 63249
3.400 7.08 1.0e-05
2026-10-16 06:10:32 EZIE-C
NORAD 63249
STARLINK-34633
NORAD 64804
2.973 13.11 8.7e-06
2026-10-16 11:21:39 EZIE-C
NORAD 63249
LEMUR-2-HOTSPUR-TOM
NORAD 66786
4.233 15.01 8.8e-08
2026-10-16 19:22:33 EZIE-C
NORAD 63249
LEMUR-2-TARTIFLETTE
NORAD 66784
4.713 15.01 7.1e-08

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite