▸Orbital parameters

Orbit class	SSO
Inclination	97.1977°
Eccentricity	0.0001656
Period	93.4 min
Apogee	444 km
Perigee	442 km
Mean motion	15.40948044 rev/day
RAAN	263.5832°
Arg of perigee	106.3145°
Mean anomaly	253.8284°
B*	1.5759e-4
Rev at epoch	4,832

▸Two-line element set (TLE)

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

1 65315U 25188A 26187.72486410 .00006403 00000-0 15759-3 0 9993

2 65315 97.1977 263.5832 0001656 106.3145 253.8284 15.40948044 48327

▸ source OMM (JSON)

{
  "OBJECT_NAME": "PELICAN-3",
  "OBJECT_ID": "2025-188A",
  "EPOCH": "2026-07-06T17:23:48.258+00:00",
  "MEAN_MOTION": 15.40948044,
  "ECCENTRICITY": 0.0001656,
  "INCLINATION": 97.1977,
  "RA_OF_ASC_NODE": 263.5832,
  "ARG_OF_PERICENTER": 106.3145,
  "MEAN_ANOMALY": 253.8284,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65315,
  "REV_AT_EPOCH": 4832,
  "BSTAR": 0.00015759,
  "MEAN_MOTION_DOT": 0.00006403,
  "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	PELICAN-3
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 26, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	160HIGHvia 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/65315

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