▸Orbital parameters

Orbit class	SSO
Inclination	97.3784°
Eccentricity	0.0002895
Period	93.4 min
Apogee	444 km
Perigee	440 km
Mean motion	15.41414253 rev/day
RAAN	272.1676°
Arg of perigee	196.3338°
Mean anomaly	163.7816°
B*	3.2894e-4
Rev at epoch	10,532

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 60514U 24149AY 26187.69953899 .00013674 00000-0 32894-3 0 9998

2 60514 97.3784 272.1676 0002895 196.3338 163.7816 15.41414253105327

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FLOCK 4BE-9",
  "OBJECT_ID": "2024-149AY",
  "EPOCH": "2026-07-06T16:47:20.169+00:00",
  "MEAN_MOTION": 15.41414253,
  "ECCENTRICITY": 0.0002895,
  "INCLINATION": 97.3784,
  "RA_OF_ASC_NODE": 272.1676,
  "ARG_OF_PERICENTER": 196.3338,
  "MEAN_ANOMALY": 163.7816,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60514,
  "REV_AT_EPOCH": 10532,
  "BSTAR": 0.00032894,
  "MEAN_MOTION_DOT": 0.00013674,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	FLOCK 4BE-9
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5.7HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/60514

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.